American Institute of Aeronautics and Astronautics. AIAA Journal 2003: Vol 41 Index

15 Pages·2003·6.1 MB·English

a
AIAA JOURNAL, VOL. 41, NO. 12: 2003 INDEX
Chronological Index
J02-085 Assessment of the Accuracy of Representing a Helical J03-007 Mechanism of Shock Wave Oscillation in Transonic
Vortex by Straight Segments. D. H. Wood and D. Li, University Diffusers. Taro Handa and Mitsuharu Masuda, Kyushu University,
of New Castle, Australia (40, 4, p.647) Article Japan; and Kazuyasu Matsuo, The University of Kitakyushu, Japan
Technical Comment by D. I. Greenwell, University of Bristol, (41, 1, p. 64) Article
England, U.K. (41, 2, p.332)
>
Reply (41, 2, p.333) J03-008 Experimental Investigation of the Flow Past a
Submarine at Angle of Drift. David Bridges, Mississippi State
J02-088 Acoustic Analogy and Alternative Theories for Jet University; and Jimmy N. Blanton, Wesley H. Brewer, and Joel T.
Noise Prediction. Philip J. Morris, Pennsylvania State University, Park, U.S. Navy William B. Morgan Large Cavitation Channel
and F. Farassat, NASA Langley Research Center (40, 4, p.671) (41, 1, p. 71) Article
Technical Comment C. K. W. Tam, Florida State University
(41, 9, p. 1844) J03-009 Fault Classification Using Pseadomodal Energies and
Reply (41, 9, p. 1845) Neural Networks. Tshilidzi Marwala, Dzinet Investment Holding,
Republic of South Africa (41, 1, p. 82) Article
J02-178 Large-Eddy Simulation of a Turbulent Compressible
Round Jet” vis-a-vis Lighthill’s Theory of Jet Noise. James R. J03-010 Multilayered Piezelectric Refined Plate Theory. Claire
DeBonis, NASA John H. Glenn Research Center; and James N. Ossadzow-David, Université Paris VI, France; and Maurice
Scott, The Ohio State University (40, 7, p.1346) Article Touratier, Ecole Nationale Supérieure, France (41, |, p. 90) Article
Technical Comment by H. S. Ribner, University of Toronto,
Canada (41, 4, p.750) J03-011 Superelastic and Shape Memory Effects in Laminated
Reply (41, 4, p.751) SMA Beams. S. Marfia, E. Sacco, Univerity of Cassino, Italy, and
J. N. Reddy, Texas A&M University (41, 1, p. 100) Article
J02-184 Structural Damage Detection by Generic Algorithms.
Kaazem Moslem and Ramin Nafaspour, Ferdowsi University, J03-012 High-Order Analysis of Unidirectional Sandwich
Tran (40,7,p.1395) Article Panels with Piezolaminated Face-Sheets and Soft Core. Oded
Technical Comment by Menahem Baruch, Technion—Israel Rabinovitch, Jack R. Vinson, University of Delaware; and Yeoshua
Institute of Technology, Israel (41, 3, p. 559) Frostig, Technion—Israel Institute of Technology, Israel
(41, 1, p. 110) Article
J02-208 Effect of Surface Roughness on Unseparated Shock-
Wave/ Boundary-Layer Interactions. H. Babinksy, University of J03-013 Structural Integrity Re-design Through Neural
Cambridge, England, UK; and G. R. Inger, lowa State University Network Inverse Mapping. R. M. Pidaparti and S. Jayanti, M. J.
(40, 8, p. 1567) Article Palakal and S. Mukhopadhyay, /ndiana University—Purdue
Errata (41, 12, p.2508) University at Indianapolis (41, 1, p. 119) Article
J03-001 Leading-Edge Vortex Structure of Nonslender Delta J03-014 New Numerical Method for Two-Dimensional
Wings at Low Reynolds Number. Michael V. Ol, U.S. Air Force Partially Wrinkled Membranes. Hongli Ding and Bingen Yang,
Research Laboratory; and Morteza Gharib, California Institute of University of Southern California, and Michael Lou and Houfei
Technology (41, 1, p. 16) Article Fang, Jet Propulsion Laboratory, California Institute of Technology
(41, 1, p. 125) Article
J03-002 Curvature Based Wall Boundary Condition for the
Euler Equations on Unstructured Grids. Z. J. Wang and Yuzhi J03-015 Viscous Supersonic Flow over Moving Compression
Sun, Michigan State University (41, 1, p. 27) Article Ramp. S. O. Park, C. H. Lee and K. M. Kang, Korea Advanced
Institute of Science and Technology, Korea (41, 1, p. 133)
J03-003 Laminarization of Turbulent Boundary Layer on Technical Note based on AIAA Paper 2001-0568
Flexible and Rigid Surfaces. Lucio Maestrello, NASA Langley
Research Center (41, 1, p. 34) Article J03-016 Modification of a Circular Near Wake by a
Rectangular Jet. D. M. Rooney, Hofstra University: and M. S.
J03-004 Generalized Logarithmic Law and Its Consequences . Gaspin, Hofstra University (41, 1, p. 137) Technical Note
Matthias H. Buschmann, Technische Universitat Dresden,
Germany, and Mohamed Gad-el-Hak, Virginia Commonwealth J03-017 Rotating Multilayer Cylindrical Shells to Impact
University (41, 1, p. 40) Article Loading. S. W. Gong and K. Y. Lam, Institute of High Performance
Computing, Singapore (41, 1, p. 139) Technical Note
J03-005 Stable Numerical Method Applying a Total Variation
Scheme for Incompressible Flow. Byeong Rog Shin, Tohoku J03-018 Recent Developments in the Research on Pulse
University, Japan (41, 1, p. 49) Article Detonation Engines. K. Kailasanath, U.S. Naval Research
Laboratory (41, 2, p. 145) Article
J03-006 Boundary Conditions for Euler Equations. Sylvie
Benzoni-Gavage and Jean-Francois Coulombel, Centre National de J03-019 Experimental and Theoretical Study on Rolling
la Recherche Scientifique, France; and Stéphane Aubert, Ecole Effectiveness of Multiple Control Surfaces. Deman Tang, Aiqin
Centrale de Lyon, France (41, 1, p. 56) Article Li, and Earl H. Dowell, Duke University (41, 2, p. 160) Article
2526 AIAA JOURNAL, VOL. 41, NO. 12: 2003 INDEX
J03-020 Low-Reynolds-Number k-€ Modeling of Non- J03-032 Flow-Tagging Velocimetry for Hypersonic Flows
stationary Solid Boundary Flows. C. B. Hwang and Using Fluorescence of Nitric Oxide. Paul M. Danehy, Sean
C. A. Lin, National Tsing Hua University, Taiwan, ROC (A, 2, O’Byrne, A. Frank P. Houwing, Jodie S. Fox, and Daniel R. Smith,
p. 168) Article Australian National University, Australia (41, 2, p. 263) Article
J03-021 Index-Matched Boundary Techniques for the J03-033 Using Aeroelastic Modes for Nonlinear Panel Flutter
Elimination of Acoustical Resonances. Jack H. Parker, U. S. Air at Arbitrary Supersonic Yawed Angle. Xinyun Guo and Chuh
Force Research Laboratory; and Bradley D. Duncan, University of Mei, Old Dominion University (41, 2, p. 272) Article
Dayton (41, 2, p. 176) Article
J03-034 Dynamic Equivalence Conditions for Controlled
J03-022 Prediction of Rod—Airfoil Interaction Noise Using the Robotic Manipulators. M. Ghanekar, Honeywell Engines,
Ffowcs-Williams-Hawkings Analogy. Damiano Casalino, Ecole Systems, and Services, Canada; and D. W.L. Wang and G. R.
Centrale de Lyon, France; Marc Jacob, Universite C. Bernard; Heppler, University of Waterloo, Canada (41, 2, p. 280) Article
Villeurvanne, France, France; and Michel Roger, Ecole Centrale
de Lyon, France (41, 2, p. 182) Article J03-035 Computational Inverse Technique for Material
Charecterization of Functionally Graded Materials. X. Han and
J03-023 Humps/Steps Influence on Stability Characteristics of G. R. Liu, National University of Singapore, Singapore (41, 2,
Two-Dimensional Laminar Boundary Layer. Anke Worner, p. 288) Article
Ulrich Rist, and Siegfried Wagner, University of Stuttgart,
Germany (41, 2, p. 192) Article
J03-036 Thermally Induced Vibrations of Spinning Thin-
Walled Composite Beam. Kyung-Eun Ko and Ji-Hwan Kim,
J03-024 Algorithm Developments for Discrete Adjoint
Seoul National University, Korea (41, 2, p. 296) Article based on
Methods. Michael B. Giles and Mihai C. Duta, Oxford University,
AIAA Paper 2002-1623
England, UK; Jens-Dominik Miiller, Queen's University, England,
UK; and Niles A. Pierce, California Instititute of Technology (41, 2,
J03-037 Structural Analysis of Pneumatic Envelopes:
p. 198) Article
Variational Formulation and Optimization-Based Solution
Process. Frank E. Baginski, George Washington University, and
J03-025 Split-Domain Harmonic Balance Sclutions to
Willi W. Schur, New Mexico State University (41, 2, p. 304) Article
Burger’s Equation for Large Amplitude Disturbances.
based on AIAA Paper 2002-1461
Raymond C. Maple, Paul I. King, U.S. Air Force Institute of
Technology; J. Mitch Wolff, Wright State University, and Paul D.
J03-038 Extrapolation Effects on Coupled Computational
Orkwis, University of Cincinnati (41, 2, p. 206) Article
Fluid Dynamics/Computational Structural Dynamics
Simulations . G. S. L. Goura, K. J. Badcock, M. A. Woodgate, and
J03-026 Numerical Simulation: Supersonic Flow Around
B. E. Richards, University of Glasgow, United Kingdom (41, 2, p.
Wing-Body Configuration with Integrated Engine Nacelle.
312) Technical Note
Masahiro Kanazaki, Shigeru Obayashi, and Kazuhiro Nakahashi,
Tohoku University, Japan (41, 2, p. 213) Article
J03-039 Vortex Interaction of a Delta Wing Flowfield. C. Shih
and Z. Ding, Florida A&M University and Florida State University
J03-027 Hybrid Reynolds-Averaged Navier—Stokes/Large-
(41, 2, p. 314) Technical Note
Eddy Simulations of Supersonic Turbulent Mixing. Nicholas J.
Georgiadis, NASA John H. Glenn Research Center; and J. twin D.
J03-040 Numerical Study of N-Wave Propagation Using
Alexander and Eli Reshotko, Case Western Reserve University
(41, 2, p. 218) Article based on AIAA Paper 2001-2563 Optimized Compact Finite Difference Schemes. In Bo Shim, and
Jae Wook Kim and Duck Joo Lee, Korea Advanced Institute of
Science and Technology, Republic of Korea (41, 2, p. 316)
J03-028 Comparisons of Initially Turbulent, Low-Velocity-
Ratio Circular and Square Coaxial Jets. Dimitris E. Technical Note
Nikitopoulos and Jason W. Bitting, Louisiana State University; and
Sivaram Gogineni, Innovative Scientific Solutions (41, 2, p. 230) J03-041 Effects of Combustion on the Sound Pressure
Article Generated by Circular Jet Flows. Kapil K. Singh, Steven H.
Frankel and Jay P. Gore, Purdue University (41, 2, p. 319)
J03-029 Lumped Element Modeling of Piezoelectric-Driven Technical Note
Synthetic Jet Actuators. Quentin Gallas, Ryan Holman, Toshikazu
Nishida, Bruce Carroll, Mark Sheplak, and Louis Cattafesta, J03-042 Wall Boundary Effects of Wire-Wrapped Cylinders at
University of Florida (41, 2, p. 240) Article High Reynolds Number. William J. Rowland and Hamid R. Rahai,
California State University (41, 2, p. 322) Technical Note
J03-030 Dezelerating Boundary Layer: A New Scaling and
Mixing Length Model. A. Bernard, J. M. Foucaut, P. Dupont, and J03-043 Oscillating Flows in a Model Pulse Detonation Engine
M. Stanislas, Laboratoire de Mécanique de Lille, France Inlet. S. Mullagiri, C. Segal, and P. J. Hubner, University of Florida
(41, 2, p. 248) Article (41, 2, p. 324) Technical Note
J03-031 Method to Improve the Accuracy of the Straight- J03-044 Differential Equation for the Amplitude of Wrinkles.
Segment Representation of Helical Vortices. D. H. Wood, Marcelo Epstein, University of Calgary, Canada (41, 2, p. 327)
University of Newcastle, Australia (41, 2, p. 256) Article Technical Note
AIAA JOURNAL, VOL. 41, NO. 12: 2003 INDEX 2527
J03-045 Contact Stress from Asymptotic Reissner—Mindlin J03-057 Hydrogen and Helium Leak Rates from
Plate Theory. Dewey H. Hodges, Georgia Institute of Technology Micromachined Orifices. I. D. Lee, O. I. Smith and A. R.
(41, 2, p. 329) Technical Note Karagozian, University of California (41, 3, p. 457) Article
J03-046 Comparison of Heat Transfer Augemtation J03-058 Nonequilibrium Radio Frequency Discharge Plasma
Techniques. P. M. Ligrani and M. M. Oliveira, University of Utah; Effect on Conical Shock Wave: M = 2.5 Flow. Peter Palm,
and T. Blaskovich, Pratt and Whitney Canada, Canada (41, 3, p. Rodney Meyer, Elke Plénjes, J. William Rich, and Igor V.
337) Survey Adamovich, The Ohio State University (41, 3, p. 465) Article
J03-047 Aeroelastic Dynamic Analysis of a Full F-16 J03-059 Optical Measurements of the Temperature in a
Configuration for Various Flight Conditions. Philippe Geuzaine, Supersonic Jet. Yann Marchesse, Yves Gervais, and Henri Foulon,
Gregory Brown, Chuck Harris, and Charbel Farhat, University of Université de Poitiers, France (41, 3, p. 470) Article
Colorado (41, 3, p. 363) Article
J03-060 Probe to Measure Direction and Strength of Moving
J03-048 Acoustics and Thrust of Quiet Separate-Flow High- Shocks or Blast Waves. Yiannis Andreopoulos, Minwei Gong,
Bypass Ratio Nozzles. Naseem H. Saiyed, NASA John H. Glenn Zhexuan Wang, and Savvas Xanthos, City College of the City
Research Center, Kevin L. Mikkelsen, Aero Systems Engineering; University of New York (41, 3, p. 476) Article
and James E. Bridges, NASA John H. Glenn Research Center
(41, 3, p. 372) Article J03-061 Aeroacoustic Instability in Rockets. Gary A. Flandro,
University of Tennessee Space Institute; and Joseph Majdalani,
Marquette University (41, 3, p. 485) Article based on AIAA Paper
J03-049 Initial-Value Problem for Hypersonic Boundary-
2001-3868
Layer Flows. Alexander Fedorov, Moscow Institute of Physics and
Technology, Russia; and Anatoli Tumin, University of Arizona
(41, 3, p. 379) Article J03-062 Improved Dynamic Flexibility Method for Extracting
Constrained Modes from Free Test Data. De-Wen Zhang, Beijing
Institute of Structure and Environment Engineering, PRC; and Fu-
J03-050 High-Resolution Large-Eddy Simulation of Flow
Shang Wei, Kaman Aerospace Corporation (41, 3, p. 498) Article
Around Low-Pressure Turbine Blade. B. Raverdy, I. Mary, and P.
Sagaut, ONERA, France; and N. Liamis, SVECMA Moteurs,
J03-063 Approximate Vibration Reanalysis of Structures. Uri
France (41, 3, p. 390) Article
Kirsch, Technion—Israel Institute of Technology, Israel
(41, 3, p. 504) Article
J03-051 Noise, Turbulence, and Thrust of Subsonic Freejets
from Lobed Nozzles. K.B.M.Q Zaman, F. Y. Wang, and N. J.
J03-064 Axial Passive Damping Testing of Mass-Produced
Georgiadis, NASA John H. Glenn Research Center at Lewis Field
Stress Coupled, Cocured Damped Composites. Angela Trego
(41, 3, p. 398) Article
and Christopher Davis, Boeing Phantom Works; and Paul F.
Eastman, Brigham Young University (41, 3, p. 512) Article
J03-052 Helmholtz-Like Resonator Self Sustained
Oscillations, Part 1: Acoustical Measurements and Analytical
J03-065 Imperfection Sensitivity of Conical Shells. Yiska
Models. S. Dequand, X. Luo, J. Willems, and A. Hirschberg,
Goldfeld, Technion-Israel Institute of Technology, Israel, Izhak
Eindhoven University of Technology, The Netherlands (41, 3, p.
Sheinman, Technion-Israel Institute of Techology, Israel; and
408) Article
Menahem Baruch, Technion—Israel Institute of Technology, Israel
(41, 3, p. 517) Article
J03-053 Helmholtz-Like Resonator Self Sustained
Oscilliations, Part 2: Detailed Flow Measurements and J03-066 New Approximate Formulas for Viscosity and
Numerical Simulations. S. Dequand, Eindhoven University of Thermal Conductivity of Dilute Gas Mixtures. Drew A.
Technology, The Netherlands, S. Hulshoff, Delft University of Copeland, The Boeing Company (41, 3, p. 525) Article
Technology, The Netherlands; and H. van Kuiyjik, J. Willems, and A.
Hirschberg, Eindhoven University of Technology, The Netherlands J03-067 Acoustic and Entropy Pulses Created in Duct Flows
(41, 3, p. 416) Article by Rapid Local Events. Miklos Sajben, University of Cincinnati
and Gary L. Cole and John W. Slater, NASA John H. Glenn
J03-054 Dynamics of an Internal Flowfield Driven by Two Research Center (41, 3, p. 538) Technical Note
Hydrodyamic Instabilities. JérGme Vétel, Frédéric Plourde, and
Son Doan-Kim, Ecole Nationale Supérieure de Mécanique et d’ J03-068 Vortex Shedding and Transition Frequencies
Aérotechnique, France (41, 3, p. 424) Article Associated with Flow Around a Circular Cylinder. N. A. Ahmed
and D. J. Wagner, University of New South Wales, Australia (41, 3,
J03-055 Structure of Flow over a Hypersonic Inlet with Side p. 542) Technical Note
Compression Wedges. Y. P. Goonko, A. F. Latypovy, I. 1. Mazhul,
A. M. Kharitonov, and M. I. Yaroslavtsev, /nstitute of Theoretical J03-069 Vortex Breakdown-Tail Interaction. Y. Kim, M.
and Applied Mechanics, Russia; and P. Rostand, Dassault Aviation, Ozgoren, and D. Rockwell, Lehigh University (41, 3, p. 544)
France (41, 3, p. 436) Article based on AIAA Paper 1998-1624 Technical Note
J03-056 Effect of Geometrical Parameters on the Mixing J03-070 Autonomous Gain-Phase Tailoring of Rotational
Performance of Cantilevered Ramp Injectors. Bernard Parent Acceleration Rate Sensors. Yu-Hsiang Hsu and Chih-Kung Lee,
and Jean P. Sislian, University of Toronto, Canada (41, 3, p. 448) National Taiwan University, Republic of China (41, 3, p. 549)
Article Technical Note
2528 AIAA JOURNAL, VOL. 41, NO. 12: 2003 INDEX
J03-071 Assessment of Delamination Fracture Load of J03-085 Trapped Vortex in Ground Effect. Darwin L. Garcia
Stringer Stiffened Composite Panel. R. Ramesh Kumar, K. S. and Joseph Katz, San Diego State University (41, 4, p. 674) Article
Praveen, and G. Venkateswara, Vikram Sarabhai Space Center,
india (41, 3, p. 551) Technical Note J03-086 Dual-Pump Coherent Anti-Stokes Raman Scattering
Temperature and CQ, Concentration Measurements. Robert P.
J03-072 Finite Element Model Updating for Helicopter Rotor Lucht and Viswanathan Velur-Natarajan, Texas A&M University;
Blade Using Genetic Algorithm. Veerabhadra Rao Akula and Campbell D. Carter, Keith D. Grinstead, and Jr., Innovative
Ranjan Ganguli, Indian Institute of Science, India (41, 3, p. 554) Scientific Solutions Inc.,; James R. Gord, U.S. Air Force Research
Technical Note
Laboratory; and Paul M. Danehy, The Australian National
University, Australia; G. J. Fiechtner and Roger L. Farrow, Sandia
J03-073 Golinski’s Speed Reducer Problem Revisited.
National Laboratories (41, 4, p. 679) Article
Tapabrata Ray, National University of Singapore, Singapore
(41, 3, p. 556) Technical Note J03-087 Evolutionary Optimization of Computationally
Expensive Problems via Surrogate Modeling. Yew S. Ong,
J03-074 Debate Concerning the Mean-Velocity Profile of a Prasanth B. Nair, and Andrew J. Keane, University of Southampton,
Turbulent Boundary Layer. Matthias H. Buschmann, Technische
England, UK (41, 4, p. 687) Article
Universitat Dresden, Germany; and Mohamed Gad-el-Hak,
Virginia Commonwealth University (41, 4, p. 565) Article
J03-088 Full-Field Three-Dimensional Volume Vibrations for
Piezoceramic Materials in Resonance. Chien-Ching Ma,
J03-075 Lessons from LESFOIL Project on Large-Eddy
National Taiwan University, Taiwan, ROC; Chi-Hung Huang,
Simulation of Flow Around an Airfoil. Christopher P. Mellen,
Ching Yun Institute of Technology, Taiwan, ROC; Hsien-Yang Lin,
Jochen Frohlich and Wolfgang Rodi, University of Karlsruhe,
De Lin Institute of Technology, Taiwan, ROC; and Chan-Chian Lin,
Germany (41, 4, p. 573) Article based on AIAA Paper 2002-0111
National Taiwan University, Taiwan, ROC (41, 4, p. 697) Article
J03-076 Accurate Multiblock Navier-Stokes Solver for
J03-089 Effective Coefficients of Piezoelectric Fiber
Complex Aerodynamic Configurations. B. Epstein, Academic
Reinforced Composites. Nilanjan Mallik and M. C. Ray, /ndian
College of Tel-Aviv-Yaffo, Israel; and T. Rubin and S. Séror, /srael
Aircraft Industries, Israel (41, 4, p. 582) Article Institute of Technology, India (41, 4, p. 704) Article
J03-077 Grid Convergence Error Analysis for Mixed-Order J03-090 Energy-Recycling Semi-Active Method for Vibration
Numerical Schemes. Christopher J. Roy, Sandia National Suppression with Piezoelectric Transducers. Junjiro Onoda,
Laboratories, USA (41, 4, p. 595) Article Institute of Space and Astronautical Science, Japan; Kanjuro
Makihara, University of Tokyo, Japan; and Kenji Minesugi, The
J03-078 Computational Simulation of the Autonomous Institute of Space and Astronautical Science, Japan (41, 4, p. 711)
Navigation of aB iomimetic Underwater Vehicle. Samuel F. Galls Article
and Othon K. Rediniotis, Texas A&M University (41, 4, p. 605)
Article J03-091 Transient Analysis of Anisotropic Multilayered Media
Subjected to Dynamic Antiplane Loadings. Yi-Shyong Ing and
J03-079 Throat Heating Effect on Critical Roughness and Chih-Chung Chen, Tamkang University, Taiwan, ROC (41, 4, p.
Nozzle Wall Boundary-Layer Stability. R. -S. Lin, V. lyer, and M. 720) Article
R. Malik, High Technology Corporation (41, 4, p. 612) Article
J03-092 Neural Networks for Inverse Problems in Damage
J03-080 Passive Mixing Control via Lobed Injectors in High- Identification and Optical Imaging. Yong Y. Kim and Rakesh K.
Speed Flow. A. J. Majamaki, O. I. Smith, and A. R. Karagozian, Kapania, Virginia Polytechnic Institute and State University (41, 4,
University of California (41, 4, p. 623) Article p. 732) Article
J03-081 Plasma Study on the Ionization of Flowing Gases by J03-093 Experimental Study of Corotating Wake-Vortex
Direct Current Electric Discharge. Stelu Deaconu, Hugh W.
Merger at Reynolds Numbers of Order 105. R. L. Bristol, J. M.
Coleman, and S. T. Wu, University of Alabama in Huntsville
Ortega, and O. Savas, University of California at Berkeley (41, 4,
(41, 4, p. 633) Article
p. 741) Technical Note
J03-082 Toward a Flame Embedding Model for Turbulent
J03-094 Reynolds-Number Correlations for Separation of
Combustion Simulation. Y. M. Marzouk and A. F. Ghoniem,
Turbulent Boundary Layers. V. A. Sandborn, Colorado State
Massachusetts Institute of Technology, and H. N. Najm, Sandia
National Laboratories (41, 4, p. 641) Article based on AIAA Paper University (41, 4, p. 744) Technical Note
2000-0866
J03-095 Contribution to the Understanding of Flow
J03-083 Low-Mach-Number Preconditioning Applied to Interactions Betweeen Multiple Synthetic Jets. Mark Watson,
Turbulent Helicopter Fuselage Flowfield Computation. Vincent Artur J. Jaworski, and Norman J. Wood, University of Manchester,
Gleize, and Michel Costes, ONERA, France (41, 4, p. 653) Article England, UK (41, 4, p. 747) Technical Note
J03-084 Two-Dimensional Model for Simulating Shock-Wave J03-096 Heat Flux Gage Studies of Compressible Dynamic
Interaction with Rigid Porous Materials. G. Malamud, D. Levi- Stall. M. S. Chandrasekhara, Naval Postgraduate School; and
Hevroni, and A. Levy, Ben-Gurion University of the Negev, Israel M. C. Wilder, NASA Ames Research Center (41, 5, p. 757) Article
(41, 4, p. 663) Article based on AIAA Paper 2002-0291
AIAA JOURNAL, VOL .. 41, NO. 12: 2003 INDEX 2529
J03-097 Efficient and Robust Reynolds-Stress Model J03-110 Convergence Properties of Analytical Target
Computation of Three-Dimensional Compressible Flows. J. C. Cascading. Nestor Michelena, University of Michigan; Hyungju
Chassaing and G. A. Gerolymos, and I. Vallet, Univeristé Pierre-et- Park, Oakland University; and Panos Y. Papalambros, University of
Marie-Curie, France (41, 5, p. 763) Article Michigan (41, 5, p. 897) Article
J03-098 Toroidal Plasma Thruster for Deep Space Flights. J03-111 Pressure-Correction Method for Low-Speed
N. N. Gorelenkov and L. E. Zakharov, Princeton University; and Pressure-Sensitive Paint Measurements. Tianshu Liu, NASA
M. V. Gorelenkova, Troitsk Institute for Innovative and Langley Research Center (41, 5, p. 906) Article
Thermonuclear Research, Russia (41, 5, p. 774) Article
J03-112 Experimental Verification of a Test-Based Hybrid
J03-099 Velocity Measurements in a Three-Dimensional Component Mode Synthesis Approach. Y. Soucy, Canadian
Compressible Base Flow. Brad A. Boswell, Sandia National Space Agency, Canada; and J. L. Humar, Carleton University,
Canada (41, 5, p. 912) Article
Laboratories, and J. Craig Dutton, University of Illinois at
Urbana-Champaign (41, 5, p. 785) Article based on AIAA Paper
J03-113 Analysis of Sandwich Plates with Viscoelastic
2002-0292
Damping Using Two-Dimensional Plate Modes. Gang Wang and
Norman M. Wereley, University of Maryland; and Der-Chen
J03-100 Helmholtz Resonator Impedance Model, Part I:
Chang, Georgetown University (41, 5, p. 924) Article based on
Nonlinear Behavior. A. S. Hersh, B. E. Walker, and J. W. Celano,
AIAA Paper 2002-1366
Hersh Walker Acoustics (41, 5, p. 795) Article
J03-114 Influence of Contact Phenomena on Embedded
J03-101 Application of Vorticity Confinement to Prediction of
Delaminations Growth in Composites. Aniello Riccio, Centro
the Flow over Complex Bodies. Y. Wenren, Flow Analysis, Inc.; Italiano Ricerche Aerospaziali, Italy; Francesco Scaramuzzino,
and M. Fan, L. Wang, M. Xiao, and J. Steinhoff, University of Seconda Universita degli Studi di Napoli, Italy; and Pierluigi
Tennessee Space Institute (41, 5, p. 809) Article Perugini, Centro Italiano Ricerche Aerospaziali, Italy (41, 5, p.
933) Article
J03-102 Preconditioning Method for Low Speed Flows.
Vittorio Puoti, Centro Italiano Ricerche Aerospaziali, Italy (41, 5, J03-115 Efficient Higher-Order Shell Theory for Laminated
p. 817) Article Composites with Multiple Delaminations. Jun-Sik Kim, /nha
University, Republic of Korea, and Maenghyo Cho, Seoul National
J03-103 Low-Reynolds-Number Turbulent Flows in Locally University, Republic of Korea (41, 5, p. 941) Article based on AIAA
Constricted Conduits: A Comparison Study. Zhe Zhang and Paper 2000-1400
Clement Kleinstreuer, North Carolina State University (41, 5, p.
831) Article J03-116 Symmetric State-Space Method for a Class of
Nonviscously Damped Systems. N. Wagner, University of
J03-104 Kinetic Equation for Particle Transport and Heat Stuttgart, Germany, and S. Adhikari, University of Cambridge,
Transfer in Nonisothermal Turbulent Flows. R. V. R. Pandya and England, UK (41, 5, p. 951) Article
F. Mashayek, University of Illinois at Chicago (41, 5, p. 841)
Article J03-117 Force Method Revisited. Ramin Sedaghati, Afzal
Suleman, Concordia University, Canada (41, 5, p. 957) Article
J03-105 LSENS: A Multipurpose Kinetics and Sensitivity
Analysis Code for Homogeneous Gas-Phase Reactions. J03-118 Retarded-Time Calculation for Moving Sources.
Michael Carley, University of Bath, England, UK (41, 5, p. 967)
K. Radhakrishnan, /nstitute for Computational Mechanics in
Technical Note
Propulsion (41, 5, p. 848) Article
J03-119 Estimation of the Flowfield from Surface Pressure
J03-106 Soot Surface Growth in Laminar Hydrocarbon/Air
Measurements in an Open Cavity. Nathan E. Murray and
Diffusion Flames. A. M. El-Leathy, F. Xu, C. H. Kim, and G. M.
Lawrence S. Ukeiley, University of Mississippi (41, 5, p. 969)
Faeth, University of Michigan (41, 5, p. 856) Article
Technical Note based on AIAA Paper 2002-2866
J03-107 Application of Proper Orthogonal Decomposition to a
J03-120 Control of a Plane Jet by Fluidic Wall Pulsing. J. C.
Supersonic Axisymmetric Jet. E. Caraballo, M. Samimy, and J.
Béra, Ecole Centrale de Lyon, France; M. Ben Chiekh, Ecole
Scott, The Ohio State University; S. Narayanan, United
Nationale d’Ingénieurs de Monastir, France, and M. Michard, G.
Technologies Research Center, and J. DeBonis, NASA John H. Comte-Bellot, and M. Sunyach, Ecole Centrale de Lyon, France
Glenn Research Center at Lewis Field (41, 5, p. 866) Article (41, 5, p. 972) Technical Note
J03-108 Prediction of Lobed Mixer Vortical Structures with a J03-121 Local Coordinate Approach in Meshless Local
k-e Turbulence Model. Hayder Salman, Gary J. Page, and James Petrov—Galerkin Method for Beam Problems. I. S. Raju, NASA
J. McGuirk, Loughborough University, England, UK (41, 5, p. 878) Langley Research Center; and D. R. Phillips, Joint Institute for
Article Advancement of Flight Science—George Washington University
(41, 5, p. 975) Technical Note
J03-109 Axisymmetric Swirling Vortical Wakes Modulated by
a Control Disk. R. F. Huang and S. C. Yen, National Taiwan J03-122 The Wright Brothers: First Aeronautical Engineers
University of Science and Technology, Republic of China and Test Pilots. F. E.C. Culick, California Institute of Technology
(41, 5, p. 888) Article (41, 6, p. 985) Survey Paper
2530 AIAA JOURNAL, VOL. 41, NO. 12: 2003 INDEX
J03-123 Aerodynamics of a Double-Element Wing in Ground J03-135 Approximate Modal Identification of Lightly
Effect. Xin Zhang and Jonathan Zerihan, University of Damped, Highly-Symmetric Bladed Disks. S. J. DiMaggio and
Southampton, England, UK (41, 6, p. 1007) Article Z. H. Duron, The Aerospace Corporation; and G. Davis, The
Boeing Company (41, 6, p. 1105) Article based on AIAA Paper
J03-124 Turbulent Dissipation-Rate Equation for 2002-1225
Compressible Flows. Krishnendu Sinha and Graham V. Candler,
University of Minnesota (41, 6, p. 1017) Article J03-136 Dynamic Substructing in the Medium-Frequency
Range. C. Soize, Université de Marne-la-Vallée, France; and S.
J03-125 Bursting Frequency Predictions for Compressible Mziou, ONERA, France (41, 6, p. 1113) Article
Turbulent Boundary Layers. William W. Liou and Yichuan Fang,
Western Michigan University (41, 6, p. 1022) Article based on J03-137 Nonlinear Vibrations of Circular Cylindrical Shells
AIAA Paper 2002-0576 with Different Boundary Conditions. Marco Amabili, Universita
di Parma, Italy (41, 6, p. 1119) Article
J03-126 Nonequilibrium Turbulent-Viscosity Model for
Supersonic Free-Shear Layer/Wall-Bounded Flows. Akira J03-138 Geometrically Exact, Intrinsic Theory for Dynamics
Yoshizawa, University of Tokyo, Japan; Hitoshi Fujiwara, National of Curved and Twisted Anisotropic Beams. Dewey H. Hodges,
Aerospace Laboratory, Japan; Fujihiro Hamba and _ Shoiti Georgia Institute of Technology (41, 6, p. 1131) Article
Nisizima, University of Tokyo, Japan; and Yukihiro Kumagai,
Japan Meteorological Agency, Japan (41, 6, p. 1029) Article J03-139 Effects of Causality and Joint Conditions on Method
of Reverberation-Ray Matrix. Ji-Feng Chen, National Chiao-
Tung University, Republic of China; and Yih-Hsing Pao, National
J03-127 PEGASUS 5: An Automated Preprocessor for
Taiwan University, Republic of China (41, 6, p. 1138) Article
Overset-Grid Computational Fluid Dynamics. Stuart E. Rogers,
NASA Ames Research Center; Norman E. Suhs, U.S. Army; and
William E. Dietz, Flow Analysis, Inc. (41, 6, p. 1037) Article based J03-140 Multiple-Timescale Analysis for Bifurcation from a
on AIAA Paper 2002-3186 Multiple-Zero Eigenvalue. Angelo Luongo and Angelo Di Egidio,
University di L’Aquila, Italy; and Achille Paolone, University of
Rome “La Sapienza”, Italy (41, 6, p. 1143) Article
J03-128 Numerical Study of Wind-Tunnel Walls Effects on
Transonic Airfoil Flow. Andrey Garbaruk, Mikhail Shur, and
J03-141 Optimal Control of Laminated Shells Using
Mikhail Strelets, St. Petersburg State Technical University, Russia;
Piezoelectric Sensor and Actuator Layers. M. C. Ray, /ndian
and Philippe R. Spalart, The Boeing Company, Russia (41, 6, p.
Institute of Technology, India (41, 6, p. 1151) Article
1046) Article
J03-142 Computational Modeling of Damage Growth in
J03-129 Navier-Stokes and Direct Simulation Monte Carlo
Composite Laminates. Shiladitya Basu and Anthony M. Waas,
Predictions for Laminar Hypersonic Separation. Christopher J.
University of Michigan, and Damodar R. Ambur, NASA Langley
Roy, and Michael A. Gallis, Timothy J. Bartel, and Jeffrey L.
Research Center (41, 6, p. 1158) Article
Payne, Sandia National Laboratories (41, 6, p. 1055) Article
J03-143 Corrosion Fatigue Through Particle Swarm
J03-130 Stochastic Inlet Conditions for Large Eddy
Optimization. R. M. Pidaparti and S. Jayanti, Indiana
Simulation of a Fully-Turbulent Jet. David J. Glaze and Steven
University—Purdue University at Indianapolis (41, 6, p. 1167)
H. Frankel, Purdue University (41, 6, p. 1064) Article based on
Article
AIAA Paper 2001-2548
J03-144 Postbuckling of Stiffened Panels Using Strut, Strip,
J03-131 Numerical Study of Mixing Enhancement by Shock
and Finite Element Methods. M. Lillico, R. Butler, and G. W.
Waves in Model Scramjet Engine. Ji-Ho Kim, Youngbin Yoon,
Hunt, University of Bath, England, UK; and A. Watson and D.
and In-Seuck Jeung, Seoul National University, Korea; Hwanil Kennedy, Cardiff University, England, UK (41, 6, p. 1172) Article
Huh, Chungnam National University, Korea; and Jeong-Yeo! Choi, based on AIAA Paper 2001-1329
Pusan National University, Korea (41, 6, p. 1074) Article
J03-145 Continuum Topology Optimization of Buckling-
J03-132 Characterisation of Aircraft Wake Vortices by Sensitive Structures. Salam Rahmatalla and Colby C. Swan,
Multiple-Lidar Triangulation. Friedrich Képp, Igor Smalikho, University of Iowa (Al, 6, p. 1180) Article
and Stephan Rahm, DLR, German Aerospace Research Center,
Germany; Agnes Dolfi and Jean-Pierre Cariou, ONERA, France; J03-146 Concept Selection Using s-Pareto Frontiers.
and Michael Harris, Robert I. Young, Kevin Weekes, and Neil Christopher A. Mattson and Achille Messac, Rensselaer
Gordon, QinetiQ Malvern, England, UK (41, 6, p. 1081) Article Polytechnic Institute (41, 6, p. 1190) Article
J03-133 System Design Through Subsystem Selection Using J03-147 Effects of Ramp Side Angle in Supersonic Mixing.
Physical Programming. Mitul Patel and Kemper E. Lewis, State T. M. Abdel-Salam, S. N. Tiwari, and T. O. Mohieldin, Old
University of New York at Buffalo; and Aniela Maria and Achille Dominion University (41, 6, p. 1199) Technical Note
Messac, Rensselaer Polytechnic Institute (41, 6, p. 1089) Article
J03-148 Irregular Phenomena of Shock Reflection Transition
J03-134 Wide-Temperature Electonically Scanned Pressure in a Conventional Supersonic Wind Tunnel. Norikazu Sudani,
Measurement Module. Frederico R. Garza, Swales Aerospace, Mamoru Sato, Toshio Karasawa, Hiroshi Kanda, and Nobuhiro
Inc. and Allan J. Zuckerwar, Qamar A. Shams, Purnell Hopson, Toda, National Aerospace Laboratory of Japan, Japan (41, 6, p.
and Jr., NASA Langley Research Center (41, 6, p. 1097) Article 1201) Technical Note
AIAA JOURNAL, VOL. 41, NO. 12: 2003 INDEX 253]
J03-149 Is There a Difference Between Aeroacoustics and J03-162 Shock/Vortex Interactions Induced by Blast Waves.
Aerodynamics? An Aeroelastician’s Viewpoint. Luigi Morino, S.-M. Liang and C.-P. Lo, National Cheng-Kung University,
Universita degli Studi di Roma “Roma Tre”, Italy (41, 7, p. 1209) Taiwan, ROC (41, 7, p. 1341) Article
Article
J03-163 Control of Supersonic Impinging Jet Flows Using
J03-150 Some Advanced Concepts in Discrete Aerodynamic Supersonic Microjets. F. S. Alvi, C. Shih, R. Elavarasan, G. Garg,
Sensitivity Analysis. Arthur C. Taylor and III, Old Dominion and A. Krothapalli, Florida A&M University and Florida State
12
University, Lawrence L. Green and Perry A. Newman, NASA University (41, 7, p. 1356) Article
Langley Research Center, and Michele M. Putko, Old Dominion
University, (41, 7, p. 1224) Article J03-164 Two Benchmarks to Assess Two-Dimensional
Theories of Sandwich, Composite Plates. E. Carrera and
J03-151 Bubble Bursting and Stall Hysteresis on a Single L. Demasi, Politecnico di Torino, Italy (41, 7, p. 1356) Article
Slotted Flap High-Life Configuration. M. Baragona, L. M. M.
Boermans, M. J. L. van Tooren, H. Bijl, and A. Beukers, De/ft J03-165 Nonlinear Asymmetric Dynamic Buckling of
University of Technology, The Netherlands (41, 7, p. 1230) Article Isotropic/Laminated Orthotropic Spherical Caps. M.
Ganapathi, S. S. Gupta, and B. P. Patel, /nstitute of Armament
J03-152 Beamforming Algorithm for Distributed Source Technology, India (41, 7, p. 1363) Article
Localization and its Application to Jet Noise. Saligrama R.
Venkatesh, Boston University, and David R. Polak and Satish J03-166 Damage Assessment of a Nonlinear Space Antenna
Narayanan, United Technologies Research Center (41, 7, p. 1238) Structure Using Quasi-Linearization Methods. William B.
Article Dunbar, California Institute of Technology; and J. B. Kosmatka,
University of California, USA (41, 7, p. 1370) Article
J03-153 Noise Characteristics of Aircraft High Lift Systems.
Y. P. Guo and M. C. Joshi, The Boeing Company, USA (41, 7, J03-167 Structural Dynamic Frequency Response Using
p. 1247) Article Combined Direct and Adjoint Reduced-Order Approximations.
Eli Livne, University of Washington; and Guillermo D. Blando,
J03-154 Optimal Transpiration Boundary Control for General Atomics Aeronautical Systems, Inc., (41, 7, p. 1377) Article
Aeroacoustics. S. Scott Collis, Kaveh Ghayour, and Matthias
Heinkenschloss, Rice University (41, 7, p. 1257) Article based on J03-168 Impact of Axial Vortices on Mixing at a High
AIAA Paper 2002-2757 Convective Mach Number. Bernard Parent and Jean P. Sislian,
University of Toronto, Canada (41, 7, p. 1386) Technical Note
J03-155 Numerical Study of Detailed Flow Affecting a Direct
Measuring Skin Friction Gage. Matthew MacLean and Joseph A. J03-169 Feedback Control of a Cylinder Wake Low-
Schetz, Virginia Polytechnic Institute and State University , USA Dimensional Model. Kelly Cohen, Stefan Siegel, Thomas
(41, 7, p. 1271) Article McLaughlin, and Eric Gillies, U.S. Air Force Academy (41, 7, p.
1389) Technical Note
J03-156 Experimental Investigation of High Enthalpy Effects
on Attachment-Line Boundary Layer Transition. Keisuke Fujii, J03-170 A Mechanism for Flame Acceleration in Narrow
National Aerospace Laboratory, Japan, and Hans G. Hornung, Tubes. James D. Ott, Combustion Research and Flow Technology;
California Institute of Technology (41, 7, p. 1282) Article Elaine S. Oran, U.S. Naval Research Laboratory, and John D.
Anderson and Jr., National Air and Space Museum (41, 7, p. 1391)
J03-157 Grid-Averaged Lagrangian Equations of Dispersed Technical Note
Phase in Dilute Two-Phase Flow. Keh-Chin Chang, Jinn-Cherng
Yang, and Muh-Rong Wang, National Cheng-Kung University, J03-171 Restatement of the Spaiart—Allmaras Eddy-Viscosity
Taiwan, Republic of China (41, 7, p. 1292) Article Model in Strain-Adaptive Formulation. T. Rung, U. Bunge,
M. Schatz, and F. Thiele, Technical University of Berlin, Germany
J03-158 Titan IVB Linear-Shaped Charge Assembly Explosive (41, 7, p. 1396) Technical Note
Train Transfer Reliability. Lien C. Yang and lan P.H. Do,
Northrop Grumman Mission Systems Sector (41, 7, p. 1304) Article J03-172 Problems of the Transoceanic Airplane. |. I. Sikorsky,
based on AIAA Paper 2001-3220 Sikorsky Aircraft (41, 7A, p. 1) Article
J03-159 Improved Turbulent Boundary-Layer Model for J03-173 Airfoil Theory for Non-Uniform Mortion. Th. Von
Shock Tubes. Eric L. Petersen, University of Central Florida; and Karman and W. R. Sears, California Institute of Technology
Ronald K. Hanson, Stanford University, (41, 7, p. 1314) Article (41, 7A, p. 5) Article
J03-160 Hydroxyl Formation Mechanisms and Models in J03-174 Some Aspects of Non-Stationary Airfoil Theory and
High-Altitude Hypersonic Flows. N. E. Gimelshein and D. A. Its Practical Application. William R. Sears, California Institute of
Levin, Pennsylvania State University; and S. F. Gimelshein, Technology (41, 7A, p. 17) Article
George Washington University (41, 7, p. 1323) Article
J03-175 The Design of High-Speed Military Airplanes.
J03-161 Properties of Particle-Generated Turbulence in the Clarence L. Johnson, Lockheed Aircraft Corporation (41, 7A, p.
Final-Decay Period. K. Lee and G. M. Faeth, University of 22) Article
Michigan; and J. -H. Chen, National Cheng-Kung University,
Taiwan, ROC (41, 7, p. 1332) Article based on AIAA Paper 2003- J03-176 Three-Dimensional Wing Flutter Analysis. Alexander
1164 H. Flax, Curtis-Wright Corporation (41, 7A, p. 30) Article
2532 AIAA JOURNAL, VOL .. 41, NO. 12: 2003 INDEX
J03-177 The Drag Problem at High Supersonic Speeds. Adolf J03-193 Engineering Relations for Friction and Heat Transfer
Busemann, National Advisory Committefeo r Aeronautics (41, 7A, to Surfaces in High Velocity Flow. E.R.G. Eckert, University of
p. 37) Article Minnesota (41, 7A, p. 256) Technical Comment/Readers Forum
J03-178 Our Heritage from Wilbur and Orville Wright. Hugh J03-194 On Turbulent Flow Near a Wall. E.R. van Driest, North
L. Dryden, National Advisory Committefeo r Aeronautics (41, 7A, American Aviation (41, 7A, p. 259) Article
p. 45) History/Lecture
J03-195 The Supersonic Blunt-Body Problem—Review and
J03-179 Turbulence and Skin Friction. Th. Von Karman, Extension. Milton D. Van Dyke, Ames Aeronautical Laboratory,
California Institute of Technology (41, 7A, p. 47) Article NACA (41, 7A, p. 265) Article
J03-180 The Fundamentals of the Statistical Theory of J03-196 Observation of High Intensity Radiation by Satellites
Turbulence. Th. Von Karman, California Institute of Technology 1958 Alpha and Gamma. J. A. van Allen, G. H. Ludwig, E. C.
(41, 7A, p. 67) Article Ray, and C. E. Mcllwain, State University of lowa (41, 7A, p. 277)
Article
J03-181 The Theory of Isotropic Turbulence. Hugh L. Dryden,
National Advisory Committee for Aeronautics (41, 7A, p. 75) J03-197 Jet Noise. M. J. Lighthill, Royal Aircraft Establishment,
Article England, UK (41, 7A, p. 282) Article
J03-182 The Statistical Theory of Isotropic Turbulence. G. I. J03-198 Stability Theory for a Pair of Trailing Vortices. S. C.
Taylor, Royal Society, England, UK (41, 7A, p. 83) Article Crow, The Boeing Company (41, 7A, p. 293) Article
J03-199 Calculation of Plane Steady Transonic Flows. Earll M.
J03-183 Laminar Boundary-Layer Oscillations and Stability
Murman and Julian D. Cole, Boeing Scientific Research
of Laminar Flow. G. B. Schubauer and H. K. Skramstad, National
Laboratories (41, 7A, p. 301) Article
Bureau of Standards (41, 7A, p. 88) Article
J03-200 Structure of Turbulent Shear Flows: A New Look.
J03-184 Supersonic Aerodynamics—Principles and
Anatol Roshko, California Institute of Technology (41, 7A, p. 309)
Applications. Theodore von Karman, (41, 7A, p. 98)
Article
History/Lecture
J03-201 An Implicit Factored Scheme for the Compressible
J03-185 Methods for Predicting Phenomena in the High-Speed
Navier-Stokes Equations. Richard M. Beam and R. F. Warming,
Flow of Gases. M. J. Lighthill, Royal Aircraft Establishment,
NASA Ames Research Center (41, 7A, p. 318) Article
England, UK (41, 7A, p. 128) Article
J03-202 A Numerical Method for Solving the Equations of
J03-186 Applications of the Theory of Free Molecule Flow to
Compressible Viscous Flow. R. W. MacCormack, NASA Ames
Aeronautics. Holt Ashley, Massachusetts Institute of Technology
Research Center (41, 7A, p. 328) Article
(41, 7A, p. 143) Article
J03-203 A Theory of Unstable Combustion in Liquid
J03-187 Temperature and Velocity Profiles in the
Propellant Rocket Systems. Martin Summerfield, Princeton
Compressible Laminar Boundary Layer with Arbitrary
University (41, 7A, p. 335) Article
Distribution of Surface Temperature. Dean R. Chapman and
Morris W. Rubesin, Ames Aeronautical Laboratory (41, 7A, p. 153)
J03-204 High-Frequency Combustion Instability in Rocket
Article
Motor with Concentrated Combustion. Luigi Crocco and Sin-]
Cheng, Princeton University (41, 7A, p. 342) Article
J03-188 The Laminar-Turbulent Transition in a Boundary
Layer—Part 1. H. W. Emmons, Harvard University (41, 7A, p.
J03-205 Laminar Heat Transfer Over Blunt-Nosed Bodies at
172) Article
Hypersonic Flight Speeds. Lester Lees, The Ramo-Wooldridge
Corporation and California Institute of Technology (41, 7A, p. 356)
J03-189 A Mixing Theory for the Interaction Between Article
Dissipative Flows and Nearly Isentropic Streams. Robert T.
Jones, Ames Aeronautical Laboratory, N.A.C.A. (41, 7A, p. 181) J03-206 Buckling of Thin-Walled Circular Cylinders Under
Article Axial Compression and Internal Pressure. Y. C. Fung and E. E.
Sechler, The Ramo-Wooldridge Corporation and California
J03-190 Theoretical Determination of the Minimum Drag of Institute of Technology (41, 7A, p. 367) Article
Airfoils at Supersonic Speeds. Robert T. Jones, Ames
Aeronautical Laboratory, N.A.C.A. (41, 7A, p. 29) Article J03-207 Theory of Stagnation Point Heat Transfer in
Dissociated Air. J. A. Fay and F. R. Riddell, Avco Research
J03-191 Turbulence in Supersonic Flow. Leslie S. Kovasznay, Laboratory (41, 7A, p. 373) Article
The Johns Hopkins University (41, 7A, p. 219) Article
J03-208 Airfoil Flow Visualization and Pressure
J03-192 Turbulent Boundary Layers in Adverse Pressure Measurements in High-Reynolds-Number Transonic Flow.
Gradients. F. H. Clauser, The John Hopkins University (41, 7A, p. Herbert Olivier, Thomas Reichel and Mitja Zechner, RWTH Aachen
238) Article University, Germany (41, 8, p. 1405) Article
AIAA JOURNAL, VOL. 41, NO. 12: 2003 INDEX
J03-209 Nonaxisymmetrical Fuselage Shape Modification for J03-221 Atomic Oxygen Degradation of Polymeric Thin Films
Drag Reduction of Low Sonic-Boom Airplane. Yoshikazu in Low Earth Orbit. G. Allegri, S. Corradi, and M. Marchetti,
Makino, Ken’ichiro Suzuki, Masayoshi Noguchi, and Kenji University of Rome “La Sapienza”, Italy; and V. Milinchuck,
Yoshida, National Aerospace Laboratory, Japan (41, 8, p. 1413) Obninks’s Institute of Nuclear Power Engineering, Russia (41. 8.
Article based on AIAA Paper 2003-557 p. 1525) Article
J03-210 Scaling of Icing Tests: A Review of Recent Progress. J03-222 Influence of Four Kinds of Gradient Magnetic Fields
R. J. Kind, Carleton University, Canada (41, 8, p. 1421) Article on a Hydrogen-—Oxygen Flame. Eisuke Yamada, Masahisa
based on AIAA Paper 2003-1216 Shinoda, Hiroshi Yamashita, and Kuniyuki Kitagawa, Nagoya
University, Japan (41, 8, p. 1535) Article
J03-211 Development of Direct-Measuring Skin Friction
Gauges for HypersonicFlight Tests. Theodore B. Smith, Joseph J03-223 Optimal Streamwise Vortices Intended for Supersonic
A. Schetz, Virginia Polytechnical Institute and State University, Mixing Enhancement. Anatoli Tumin, University of Arizona
and Trong T. Bui, NASA Dryden Flight Research Center (41, 8, (41, 8, p. 1542) Article based on AIAA Paper 2002-0728
p. 1429) Article based on AIAA Paper 2002-3134
J03-224 Sandwich-Plate Vibration Analysis: Three-Layer Quasi-
J03-212 Ultrasound Technique for Prediction of Statistical Three-Dimensional Finite Element Model. Airton Nabarrete,
Characteristics of Grid-Generated Turbulence. T. A. Andreeva Centro Universitario Fundagao Educacional Inaciana Pe Sabéia de
and W. W. Durgin, Worcester Polytechnic Institute (41, 8, p. 1438) Medeiros, Brazil; Sergio Franscino M. de Almeida, /nstituto
Article based on AIAA Paper 2002-0921 Tecnolégico de Aerondutica, Brazil; and Jorn S. Hansen, University of
Toronto, Canada (41, 8, p. 1547) Article
J03-213 Correlating Friction Velocity In Turbulent Boundary
J03-225 Vibration Testing and Finite Element Analysis of an
Layers Subjected To Freestream Turbulence. Michael J. Barrett,
Inflatable Structure. Gyuhae Park, Marion Sausse, and Daniel J.
Valparaiso University; and D. Keith Hollingsworth, University of
Inman, Virginia Polytechnic Institute and State University; and
Houston, (41, 8, p. 1444) Article
John A. Main, University of Kentucky (41, 8, p. 1556) Article
J03-214 Large-Eddy Simulation of Supersonic Cavity
J03-226 Hyperveiocity Impacts on Thin Metallic and
Flowfields Including Flow Control. Donald P. Rizzetta, and
Composite Space Debris Bumper Shields. Djameel Ramjaun,
Miguel R. Visbal, U.S. Air Force Research Laboratory (41, 8,
Ichiro Kato, and Kazuyoshi Takayama, Tohoku Universwity, Japan;
p. 1452) Article based on AIAA Paper 2002-2853
and Gopalan Jagadeesh, Indian Institute of Science, India (41, 8,
p. 1564) Article
J03-215 Hybrid Simulation Approach for Cavity Flows:
Blending, Algorithm, and Boundary Treatment Issues. R. A.
J03-227 Reliability-Based Structural Optimization of an
Baurle and C.-J. Tam, Taitech, Inc.: and J.R. Edwards and H.A.
Elastic-Plastic Beam. Mazen A. Ba-abbad and Rakesh K. Kapania,
Hassan, North Carolina State University (41, 8, p. 1463) Article
Virginia Polytechnic Institute and State University; and Efstratios
based on AIAA Paper 2001-2562 <72
Nikolaidis, University of Toledo (41, 8, p. 1573) Article
Erratum (41, 10, p.2079)
J03-228 Particle Swarm Optimization. Gerhard Venter,
J03-216 Inflow Boundary Conditions for Hybrid Large
Vanderplaats Research and Development, Inc.; and Jaroslaw
Eddy/Reynolds Averaged Navier—Stokes Simulations. Xudong
Sobieszczanski-Sobieski, NASA Langley Research Center (41, 8,
Xiao, J. R. Edwards, and H. A. Hassan, North Carolina State
p. 1583) Article
University; and R. A. Baurle, Taitech, Inc. (41, 8, p. 1481) Article
based on AIAA Paper 2003-0079
J03-229 Automated Generation of High-Order Partial
Derivative Models. James D. Turner, Amdyn Systems (41, 8,
J03-217 Sectional Flow Structures in Near Wake of Elevated p. 1590) Article
Jets in a Crossflow. Rong F. Huang, and Ren H. Hsieh, National
Taiwan University of Science and Technology, Taiwan, ROC (41, 8, J03-230 Effect of Acoustic Excitation on Airfoil Performance
p. 1490) Article at Low Reynolds Numbers. Serhiy Yarusevych, University of
Toronto, Canada, John Gregory Kawall, Ryerson University,
J03-218 Spring-Supported Cylinder Wake Control. M. M. Canada; and Pierre Edward Sullivan, University of Toronto,
Zhang, and Y. Zhou and L. Cheng, The Hong Kong Polytechnic Canada (41, 8, p. 1599) Technical Note
University, PRC (41, 8, p. 1500) Article
J03-231 Robust-Optimal Design of a Lightweight Space
J03-219 Curvature Effects in Burke-Schumann Spray Flame Structure Using a Genetic Algorithm. D. K. Anthony and A. J.
Extinction. J.B. Greenberg, and F. Grodek, Technion—lIgrael Keane, University of Southampton, England, UK (41, 8, p. 1601)
Institute of Technology, Israel (41, 8, p. 1507) Article based on Technical Note
AIAA Paper 2002-0623
J03-232 Illustration of the Inclusion of Sound—Flow
J03-220 Surface Properties During Primary Breakup of Interactions in Lighthill’s Equation. Christophe Bogey, Xavier
Turbulent Liquid Jets in Still Air. K. A. Sallam and G. M. Faeth, Gloerfelt, and Christophe Bailly, Ecole Centrale de Lyon, France
University of Michigan (41, 8, p. 1514) Article (41, 8, p. 1604) Article
2534 AIAA JOURNAL, VOL. 41, NO. 12: 2003 INDEX
J03-233 Effect of Artificial Dissipation on Large-Eddy J03-246 Wall Pressure Fluctuations in a Turbulent Boundary
Simulation with Deconvolution Modeling. R. von Kaenel, ETH Layer After Blowing or Suction. Joongnyon Kim, Kyoungyoun
Ziirich, Switzerland, N. A. Adams, Technical University of Kim and Hyung Jin Sung, Korea Advanced Institute of Science and
Dresden, Germany; L. Kleiser, ETH Ziirich; and J. B. Vos, CFS Technology, Korea (41, 9, p. 1697) Article
Engineering SA, Switzerland (41, 8, p. 1606) Technical Note
J03-247 Adaptive Harmonic Balance Solutions te Euler’s
J03-234 The Accuracy of Higher Order Finite Difference Equation. Raymond C. Maple, Paul I. King and Mark E. Oxley,
Schemes on Nonuniform Grids. Yongmann M. Chung and Paul Air Force Institute of Technology (41, 9, p. 1705) Article
G. Tucker, University of Warwick, England, UK (41, 8, p. 1609)
Technical Note J03-248 Trailing Edge Cavity Afterbodies for Linear Plug
Nozzle Engines. Menko E. N. Wisse and Willem J. Bannink, De/ft
J03-235 Vibration—Dissociation Coupling Model for University of Technology, The Netherlands (41, 9, p. 1715) Article
Hypersonic Blunt-Body Flow. Eswar Josyula, U.S. Air Force based on AIAA Paper 2001-1892
Research Laboratory; and William F. Bailey, U.S. Air Force
Institute of Technology (41, 8, p. 1611) Technical Note based on J03-249 Flourescence Imaging of Rotational and Vibrational
AIAA Paper 2001-2733 Temperature in a Shock-Tunnel Nozzle Flow. Philip C. Palma,
Paul M. Danehy, and A. F. P. Houwing, Australian National
J03-236 Laser Doppler Anemometry Study of a Turbulent Jet University, Australia (41, 9, p. 1722) Article
in Crossflow. Oktay Ozcan, Yildiz Techical University, Turkey; and
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(41, 8, p. 1614) Technical Note George Constantinescu, Matthieu Chapelet, and Kyle D. Squires,
Arizona State University (41, 9, p. 1733) Article
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Ames Wind Tunnels. Norbert M. Ulbrich, Sverdrup Technology J03-251 Inverse-Imaging Method for Detection of a Vortex in
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North Carolina State University (41, 8, p. 1619) Technical Note Genetic Algorithms. S. Gunawan, S. Azarm, and J. Wu, University
of Maryland; and A. Boyars, U.S. Naval Surface Warfare Center
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Component Mode Synthesis Techniques. Ronnie Bladh,
Christophe Pierre and Matthew P. Castanier, University of J03-253 Particle Velocity on Solid-Propellant Surface Using X-
Michigan (41, 8, p. 1621) Technical Note Ray Real-Time Radiography. Yumin Xiao, R. S. Amano,
University of Wisconsin—Milwaukee; and Timin Cai, Jiang Li, and
J03-240 Development of Comprehensive Detailed and Guogiang He, Northwestern Polytechnical University (41, 9,
Reduced Reaction Mechanisms for Combustion Modeling. p. 1763) Article based on AIAA Paper 2001-1096
C. K. Law, Princeton University; C. J. Sung, Case Western Reserve
University; H. Wang, University of Delaware; and T. F. Lu, J03-254 Dynamic Analysis of Composite Laminates with
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2002-0331 Heung Soo Kim, Aditi Chattopadhyay, and Anindya Ghoshal,
Arizona State University (41, 9, p. 1771) Article
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Aerospaziali, Italy; and Renato Tognaccini, Universita degli Studi Mass Position. D. Wang, and J.S. Jiang and W.H. Jhang,
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Article
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and Steven M. Arnold, NASA John H. Glenn Research Center at
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M.K. Chock and Rakesh K. Kapania, Virginia Polytechnic Institute 1567
and State University (41, 9, p. 1667) Article based on AIAA Paper
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K. Viswanathan, The Boeing Company (41, 9, p. 1674) Article Institute of Technology (41, 9, p. 1797) Article
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Equation” Model of Turbulent Flows. Tianliang Yang, J. M. Nacional de Pesquisas Espaciais, Brazil, Pedro Paglione, and
McDonough and J. D. Jacob, University of Kentucky (41, 9, Roberto M. Girardi, /nstituto Technologico de Aerondutica, Brazil
p. 1690) Article based on AIAA Paper 2002-2962 (41, 9, p. 1808) Article