Table Of Content

2002 ANNUAL INDEX Civil Engineering Database Keyword Index The Civil Engineering Database (CEDB) is Bolted joints Damage designed to provide free, easy bibliographic Comparative Behavior of Single-Bolted and Fully Coupled Micro/Macro Deformation, access to all ASCE publications. The database Dual-Bolted Lap Joints. — John D. Pratt and Damage, and Failure Prediction for SiC/Ti-15- covers ASCE documents published since 1972. It Gerard Pardoen; 15(2), 55-63 (2002). 3 Laminates. — Brett A. Bednarcyk and provides access to all the journals, conference Influence of Head Geometry on Bolted Joint Steven M. Arnold; 15(3), 74-83 (2002) proceedings, books, standards, manuals Behavior. — John D. Pratt and Gerard Effective Strategy for Automated Characterization magazines, and newspapers. The index terms Pardoen; 15(4), 136-53 (2002). in Complex Viscoelastoplastic and Damage below were assigned to papers published in this Bolts Modeling for Isotropic/Anisotropic Aerospace journal during 2002 from a CEDB keyword Numerical Modeling of Bolted Lap Joint Materials. — A. F. Saleeb, T. E. Wilt, D. A. list. The CEDB and keyword list can be accessed Behavior. — John D. Pratt and Gerard Trowbridge, and A. S. Gendy; 15(3), 84-96 on the Web = at http://www. pubs.asce.org/ Pardoen; 15(1), 20-31 (2002). (2002). cedbsrch.html. Buckling Damping Stability of Curved Composite Panels with Active Vibration Damping of Composite Beam Acceleration Random Material Properties. — Bhrigu N using Smart Sensors and Actuators. — G Acceleration Feedback-Based Active and Passive Singh, N. G. R. Iyengar, and Dayanand Yadav; Song, P. Z. Qiao, W. K. Binienda, and G. P. Vibration Control of Landing Gear 15(2), 46-54 (2002). Zou; 15(3), 97-103 (2002) Components. — Seung-Keon Kwak, Gregory Nonlinear Buckling of Composite Shells of Deformation Washington, and Rama K. Yedavalli; 15(1), 1-9 Revolution. — Jinsong Huang; 15(2), 64-71 Fully Coupled Micro/Macro Deformation, (2002). (2002). Damage, and Failure Prediction for SiC/Ti-15- Aerodynamics Buildings, hotels 3 Laminates. — Brett A. Bednarcyk and Fluid Mechanism of Wing Rock for Space Hotels: Civil Engineering’s New Frontier. Steven M. Arnold; 15(3), 74-83 (2002). — Patrick Collins; 15(1), 10-9 (2002). Effective Strategy for Automated Characterization Configurations with Chine-Shaped Forebodies. in Complex Viscoelastoplastic and Damage — Ahmed A. Saad, Brad S. Liebst, and Composite materials Modeling for Isotropic/Anisotropic Aerospace Raymond E. Gordnier; 15(4), 125-35 (2002). Stability of Curved Composite Panels with Materials. — A. F. Saleeb, T. E. Wilt, D. A. Random Material Properties. Bhrigu N. Aerospace engineering Trowbridge, and A. S. Gendy; 15(3), 84-96 Singh, N. G. R. Iyengar, and Dayanand Yadav; Numerical Modeling of Bolted Lap Joint (2002) 15(2), 46-54 (2002). Behavior. — John D. Pratt and Gerard Nonlinear Buckling of Composite Shells of Design Pardoen; 15(1), 20-31 (2002) Revolution. Jinsong Huang; 15(2), 64-71 Engineering, Design and Construction of Lunar Comparative Behavior of Single-Bolted and (2002) Bases. — Haym Benaroya, Leonhard Bernold, Dual-Bolted Lap Joints. — John D. Pratt and Active Vibration Damping of Composite Beam and Koon Meng Chua; 15(2), 33-45 (2002). Gerard Pardoen; 15(2), 55-63 (2002). using Smart Sensors and Actuators. — G. Engines Influence of Head Geometry on Bolted Joint Song, P. Z. Qiao, W. K. Binienda, and G. P. Impact Testing and Analysis of Composites for Behavior. — John D. Pratt and Gerard Zou; 15(3), 97-103 (2002). Aircraft Engine Fan Cases. — Gary D Pardoen; 15(4), 136-53 (2002). Thermomechanical Response Variability of Roberts, Duane M. Revilock, Wieslaw K. Aircraft Stiffened Composite Panels. — Ahmed K. Binienda, Walter Z. Nie, S. Ben Mackenzie, Acceleration Feedback-Based Active and Passive Noor, James H. Starnes, Jr., and Jeanne M. and Kevin B. Todd; 15(3), 104-10 (2002). Vibration Control of Landing Gear Peters; 15(4), 154-64 (2002). Failure Components. — Seung-Keon Kwak, Gregory Composite structures Fully Coupled Micro/Macro Deformation, Washington, and Rama K. Yedavalli; 15(1), 1-9 Impact Testing and Analysis of Composites for Damage, and Failure Prediction for SiC/Ti-15- (2002). Aircraft Engine Fan Cases. — Gary D. 3 Laminates. — Brett A. Bednarcyk and Numerical Modeling of Bolted Lap Joint Roberts, Duane M. Revilock, Wieslaw K. Steven M. Arnold; 15(3), 74-83 (2002). Behavior. — John D. Pratt and Gerard Binienda, Walter Z. Nie, S. Ben Mackenzie, Fans Pardoen; 15(1), 20-31 (2002). and Kevin B. Todd; 15(3), 104-10 (2002) Impact Testing and Analysis of Composites for Comparative Behavior of Single-Bolted and Construction Aircraft Engine Fan Cases. — Gary D. Dual-Bolted Lap Joints. — John D. Pratt and Engineering, Design and Construction of Lunar Roberts, Duane M. Revilock, Wieslaw K. Gerard Pardoen; 15(2), 55-63 (2002). Bases. — Haym Benaroya, Leonhard Bernold, Binienda, Walter Z. Nie, S. Ben Mackenzie, Influence of Head Geometry on Bolted Joint and Koon Meng Chua; 15(2), 33-45 (2002) and Kevin B. Todd; 15(3), 104-10 (2002). Behavior. — John D. Pratt and Gerard Containment Fasteners Pardoen; 15(4), 136-53 (2002). Impact Testing and Analysis of Composites for Influence of Head Geometry on Bolted Joint Beams Aircraft Engine Fan Cases. — Gary D. Behavior. — John D. Pratt and Gerard Active Vibration Damping of Composite Beam Roberts, Duane M. Revilock, Wieslaw K. Pardoen; 15(4), 136-53 (2002) using Smart Sensors and Actuators G. Binienda, Walter Z. Nie, S. Ben Mackenzie, Finite element method Song, P. Z. Qiao, W. K. Binienda, and G. P. and Kevin B. Todd; 15(3), 104-10 (2002). Numerical Modeling of Bolted Lap Joint Zou; 15(3), 97-103 (2002). Core Behavior. — John D. Pratt and Gerard Integrity of Sandwich Panels and Beams with Integrity of Sandwich Panels and Beams with Pardoen; 15(1), 20-31 (2002). Truss-Reinforced Cores. — C. Kocher, W. Truss-Reinforced Cores. — C. Kocher, W. Influence of Head Geometry on Bolted Joint Watson, M. Gomez, I. Gonzalez, and V. Watson, M. Gomez, I. Gonzalez, and V. Behavior. — John D. Pratt and Gerard Birman; 15(3), 111-7 (2002). Birman; 15(3), 111-7 (2002). Pardoen; 15(4), 136-53 (2002). JOURNAL OF AEROSPACE ENGINEERING / OCTOBER 2002 / 167 Finite elements Nonlinear response Space colonies Comparative Behavior of Single-Bolted and Thermomechanical Response Variability of Space Hotels: Civil Engineering’s New Frontier. Dual-Bolted Lap Joints. — John D. Pratt and Stiffened Composite Panels. — Ahmed K. — Patrick Collins; 15(1), 10-9 (2002). Gerard Pardoen; 15(2), 55-63 (2002). Noor, James H. Starnes, Jr., and Jeanne M. Stability Fluid mechanics Peters; 15(4), 154-64 (2002). Nonlinear Buckling of Composite Shells of Fluid Mechanism of Wing’ Rock _ for Configurations with Chine-Shaped Forebodies. Numerical models Revolution. — Jinsong Huang; 15(2), 64-71 — Ahmed A. Saad, Brad S. Liebst, and Numerical Modeling of Bolted Lap Joint (2002). Raymond E. Gordnier; 15(4), 125-35 (2002). Behavior. — John D. Pratt and Gerard Integrity of Sandwich Panels and Beams with Impact tests Pardoen; 15(1), 20-31 (2002). Truss-Reinforced Cores. — C. Kocher, W. Impact Testing and Analysis of Composites for Fluid Mechanism of Wing’ Rock _ for Watson, M. Gomez, I. Gonzalez, and V. Aircraft Engine Fan Cases. — Gary D. Configurations with Chine-Shaped Forebodies. Birman; 15(3), 111-7 (2002). Roberts, Duane M. Revilock, Wieslaw K. — Ahmed A. Saad, Brad S. Liebst, and Stiffening Binienda, Walter Z. Nie, S. Ben Mackenzie, Raymond E. Gordnier; 15(4), 125-35 (2002). Thermomechanical Response’ Variability of and Kevin B. Todd; 15(3), 104-10 (2002). Joints Optimization Stiffened Composite Panels. — Ahmed K. Numerical Modeling of Bolted Lap Joint Effective Strategy for Automated Characterization Noor, James H. Starnes, Jr., and Jeanne M. Behavior. — John D. Pratt and Gerard in Complex Viscoelastoplastic and Damage Peters; 15(4), 154-64 (2002). Pardoen; 15(1), 20-31 (2002). Modeling for Isotropic/Anisotropic Aerospace Temperature Laminates Materials. — A. F. Saleeb, T. E. Wiit, D. A. Thermal Diffusion and Associated Stress Field Fully Coupled Micro/Macro Deformation, Trowbridge, and A. S. Gendy; 15(3), 84-96 due to High Speed Source. — William P. Damage, and Failure Prediction for SiC/Ti-15- (2002). Baker, Anthony N. Palazotto, and David J. 3 Laminates. — Brett A. Bednarcyk and Steven M. Arnold; 15(3), 74-83 (2002). Oscillation Laird; 15(3), 118-24 (2002). Loads Fluid Mechanism of Wing’ Rock _ for Thermal diffusion Thermomechanical Response Variability of Configurations with Chine-Shaped Forebodies. Thermal Diffusion and Associated Stress Field Stiffened Composite Panels. Ahmed K. — Ahmed A. Saad, Brad S. Liebst, and due to High Speed Source. — William P. Noor, James H. Starnes, Jr., and Jeanne M. Raymond E. Gordnier; 15(4), 125-35 (2002). Baker, Anthony N. Palazotto, and David J. Peters; 15(4), 154-64 (2002). Panels Laird; 15(3), 118-24 (2002). Material properties Stability of Curved Composite Panels with Thermal factors Stability of Curved Composite Panels with Random Material Properties. Bhrigu N. Random Material Properties. — Bhrigu N. Thermomechanical Response Variability of Singh, N. G. R. Iyengar, and Dayanand Yadav; Singh, N. G. R. Iyengar, and Dayanand Yadav; Stiffened Composite Panels. — Ahmed K. 15(2), 46-54 (2002). 15(2), 46-54 (2002). Noor, James H. Starnes, Jr., and Jeanne M. Effective Strategy for Automated Characterization Thermomechanical Response Variability of Peters; 15(4), 154-64 (2002). in Complex Viscoelastoplastic and Damage Stiffened Composite Panels. — Ahmed K. Trusses Modeling for Isotropic/Anisotropic Aerospace Noor, James H. Starnes, Jr., and Jeanne M. Integrity of Sandwich Panels and Beams with Materials. — A. F. Saleeb, T. E. Wilt, D. A. Peters; 15(4), 154-64 (2002). Truss-Reinforced Cores. — C. Kocher, W. Trowbridge, and A. S. Gendy; 15(3), 84-96 (2002). Prediction Watson, M. Gomez, I. Gonzalez, and V. Mesh generation Fully Coupled Micro/Macro Deformation, Birman; 15(3), 111-7 (2002). Influence of Head Geometry on Bolted Joint Damage, and Failure Prediction for SiC/Ti-15- Vibration Behavior. — John D. Pratt and Gerard 3 Laminates. — Brett A. Bednarcyk and Active Vibration Damping of Composite Beam Pardoen; 15(4), 136-53 (2002) Steven M. Arnold; 15(3), 74-83 (2002). using Smart Sensors and Actuators. — G. Methodology Sandwich panels Song, P. Z. Qiao, W. K. Binienda, and G. P. Acceleration Feedback-Based Active and Passive Integrity of Sandwich Panels and Beams with Zou; 15(3), 97-103 (2002). Vibration Control of Landing Gear Components. Seung-Keon Kwak, Gregory Truss-Reinforced Cores. — C. Kocher, W. Vibration control Washington, and Rama K. Yedavalli; 15(1), 1-9 Watson, M. Gomez, I. Gonzalez, and V. Acceleration Feedback-Based Active and Passive (2002). Birman; 15(3), 111-7 (2002). Vibration Control of Landing Gear Models Sensitivity analysis Components. — Seung-Keon Kwak, Gregory Thermal Diffusion and Associated Stress Field Thermomechanical Response Variability of Washington, and Rama K. Yedavalli; 15(1), 1-9 due to High Speed Source. — William P. Stiffened Composite Panels. — Ahmed K. (2002). Baker, Anthony N. Palazotto, and David J. Noor, James H. Starnes, Jr., and Jeanne M. Viscoplasticity Laird; 15(3), 118-24 (2002). Moon Peters; 15(4), 154-64 (2002). Effective Strategy for Automated Characterization Engineering, Design and Construction of Lunar Sensors in Complex Viscoelastoplastic and Damage Bases. — Haym Benaroya, Leonhard Bernold, Active Vibration Damping of Composite Beam Modeling for Isotropic/Anisotropic Aerospace and Koon Meng Chua; 15(2), 33-45 (2002). using Smart Sensors and Actuators. — G. Materials. — A. F. Saleeb, T. E. Wilt, D. A. Nonlinear analysis Song, P. Z. Qiao, W. K. Binienda, and G. P. Trowbridge, and A. S. Gendy; 15(3), 84-96 Comparative Behavior of Single-Bolted and Zou; 15(3), 97-103 (2002). (2002). Dual-Bolted Lap Joints. — John D. Pratt and Gerard Pardoen; 15(2), 55-63 (2002). Shells Influence of Head Geometry on Bolted Joint Nonlinear Buckling of Composite Shells of Behavior. — John D. Pratt and Gerard Revolution. — Jinsong Huang; 15(2), 64-71 Pardoen; 15(4), 136-53 (2002). (2002). 168 / JOURNAL OF AEROSPACE ENGINEERING / OCTOBER 2002 2002 ANNUAL INDEX Author Index Arnold, Steven M. Aerospace Materials” by A. F. Saleeb, T. E. Wilt, Nie, Walter Z. Fully Coupled Micro/Macro Deformation, Dam- D. A. Trowbridge, and A. S. Gendy. — A. F. Sa- Impact Testing and Analysis of Composites for Air- age, and Failure Prediction for SiC/Ti-15-3 leeb, T. E. Wilt, D. A. Trowbridge, and A. S. craft Engine Fan Cases. — Gary D. Roberts, Laminates. — Brett A. Bednarcyk and Steven Gendy; 15(4), 166 (2002). Duane M. Revilock, Wieslaw K. Binienda, M. Arnold; 15(3), 74-83 (2002). Gomez, M. Walter Z. Nie, S. Ben Mackenzie, and Kevin B. Baker, William P. Integrity of Sandwich Panels and Beams with Todd; 15(3), 104-10 (2002). Thermal Diffusion and Associated Stress Field due Truss-Reinforced Cores. — C. Kocher, W. Wat- Noor, Ahmed K. to High Speed Source. — William P. Baker, An- son, M. Gomez, I. Gonzalez, and V. Birman; Thermomechanical Response Variability of Stiff- thony N. Palazotto, and David J. Laird; 15(3), 15(3), 111-7 (2002). ened Composite Panels. — Ahmed K. Noor, 118-24 (2002). Gonzalez, I. James H. Starnes, Jr., and Jeanne M. Peters; Bednarcyk, Brett A. Integrity of Sandwich Panels and Beams with 15(4), 154-64 (2002). Fully Coupled Micro/Macro Deformation, Dam- Truss-Reinforced Cores. — C. Kocher, W. Wat- Palazotto, Anthony N. age, and Failure Prediction for SiC/Ti-15-3 son, M. Gomez, I. Gonzalez, and V. Birman; Review of Pressure Vessels, by Carl T. F. Ross. — Laminates. — Brett A. Bednarcyk and Steven 15(3), 111-7 (2002). Anthony N. Palazotto; 15(1), 32 (2002). M. Arnold; 15(3), 74-83 (2002). Gordnier, Raymond E. Thermal Diffusion and Associated Stress Field due Benaroya, Haym Fluid Mechanism of Wing Rock for Configurations to High Speed Source. — William P. Baker, An- Engineering, Design and Construction of Lunar with Chine-Shaped Forebodies. — Ahmed A. thony N. Palazotto, and David J. Laird; 15(3), Bases. — Haym Benaroya, Leonhard Bernold, Saad, Brad S. Liebst, and Raymond E. Gordnier; 118-24 (2002). and Koon Meng Chua; 15(2), 33-45 (2002). 15(4), 125-35 (2002). Pardoen, Gerard Bernold, Leonhard Haftka, Raphael Numerical Modeling of Bolted Lap Joint Behavior. Engineering, Design and Construction of Lunar Review of Computer aided optimum design of — John D. Pratt and Gerard Pardoen; 15(1), Bases. — Haym Benaroya, Leonhard Bernold, structures VII by S. Hernandez and C. A. 20-31 (2002). and Koon Meng Chua; 15(2), 33-45 (2002). Brebbia. — Raphael Haftka; 15(4), 165 (2002). Comparative Behavior of Single-Bolted and Dual- Binienda, W. K. Huang, Jinsong Bolted Lap Joints. — John D. Pratt and Gerard Advanced Techniques of Analysis and Testing of Nonlinear Buckling of Composite Shells of Pardoen; 15(2), 55-63 (2002). Composites for Aerospace Applications. — W. Revolution. — Jinsong Huang; 15(2), 64-71 Influence of Head Geometry on Bolted Joint K. Binienda and M.-J. Pindera; 15(3), 73 (2002). (2002). Behavior. — John D. Pratt and Gerard Pardoen; Active Vibration Damping of Composite Beam 15(4), 136-53 (2002). Iyengar, N. G. R. using Smart Sensors and Actuators. — G. Song, Stability of Curved Composite Panels with Ran- Peters, Jeanne M. P. Z. Qiao, W. K. Binienda, and G. P. Zou; 15(3), dom Material Properties. — Bhrigu N. Singh, N. Thermomechanical Response Variability of Stiff- 97-103 (2002). G. R. Iyengar, and Dayanand Yadav; 15(2), ened Composite Panels. — Ahmed K. Noor, Binienda, Wieslaw K. 46-54 (2002). James H. Starnes, Jr., and Jeanne M. Peters; Impact Testing and Analysis of Composites for Air- 15(4), 154-64 (2002). craft Engine Fan Cases. — Gary D. Roberts, Kocher, C. Duane M. Revilock, Wieslaw K. Binienda, Integrity of Sandwich Panels and Beams with Pindera, M.-J. Walter Z. Nie, S. Ben Mackenzie, and Kevin B. Truss-Reinforced Cores. — C. Kocher, W. Wat- Advanced Techniques of Analysis and Testing of Todd; 15(3), 104-10 (2002). son, M. Gomez, I. Gonzalez, and V. Birman; Composites for Aerospace Applications. — W. 15(3), 111-7 (2002). K. Binienda and M.-J. Pindera; 15(3), 73 (2002). Birman, V. Integrity of Sandwich Panels and Beams with Kwak, Seung-Keon Pratt, John D. Truss-Reinforced Cores. — C. Kocher, W. Wat- Acceleration Feedback-Based Active and Passive Numerical Modeling of Bolted Lap Joint Behavior. son, M. Gomez, I. Gonzalez, and V. Birman; Vibration Control of Landing Gear Components. — John D. Pratt and Gerard Pardoen; 15(1), 15(3), 111-7 (2002). — Seung-Keon Kwak, Gregory Washington, 20-31 (2002). and Rama K. Yedavalli; 15(1), 1-9 (2002). Comparative Behavior of Single-Bolted and Dual- Chua, Koon Meng Engineering, Design and Construction of Lunar Laird, David J. Bolted Lap Joints. — John D. Pratt and Gerard Bases. — Haym Benaroya, Leonhard Bernold, Thermal Diffusion and Associated Stress Field due Pardoen; 15(2), 55-63 (2002). and Koon Meng Chua; 15(2), 33-45 (2002). to High Speed Source. — William P. Baker, An- Influence of Head Geometry on Bolted Joint thony N. Palazotto, and David J. Laird; 15(3), Behavior. — John D. Pratt and Gerard Pardoen; Collins, Patrick 118-24 (2002). 15(4), 136-53 (2002). Space Hotels: Civil Engineering’s New Frontier. — Patrick Collins; 15(1), 10-9 (2002). Liebst, Brad S. Qiao, P. Z. Gendy, A. S. Fluid Mechanism of Wing Rock for Configurations Active Vibration Damping of Composite Beam Effective Strategy for Automated Characterization with Chine-Shaped Forebodies. — Ahmed A. using Smart Sensors and Actuators. — G. Song, in Complex Viscoelastoplastic and Damage Saad, Brad S. Liebst, and Raymond E. Gordnier; P. Z. Qiao, W. K. Binienda, and G. P. Zou; 15(3), Modeling for Isotropic/Anisotropic Aerospace 15(4), 125-35 (2002). 97-103 (2002). Materials. — A. F. Saleeb, T. E. Wilt, D. A. Mackenzie, S. Ben Revilock, Duane M. Trowbridge, and A. S. Gendy; 15(3), 84-96 Impact Testing and Analysis of Composites for Air- Impact Testing and Analysis of Composites for Air- (2002). craft Engine Fan Cases. — Gary D. Roberts, craft Engine Fan Cases. — Gary D. Roberts, Errata for “Effective Strategy for Automated Char- Duane M. Revilock, Wieslaw K. Binienda, Duane M. Revilock, Wieslaw K. Binienda, acterization in Complex Viscoelastoplastic and Walter Z. Nie, S. Ben Mackenzie, and Kevin B. Walter Z. Nie, S. Ben Mackenzie, and Kevin B. Damage Modeling for Isotropic/Anisotropic Todd; 15(3), 104-10 (2002). Todd; 15(3), 104-10 (2002). JOURNAL OF AEROSPACE ENGINEERING / OCTOBER 2002 / 169 Roberts, Gary D. Starnes, James H., Jr. Wilt, T. E. Impact Testing and Analysis of Composites for Air- Thermomechanical Response Variability of Stiff- Effective Strategy for Automated Characterization craft Engine Fan Cases. — Gary D. Roberts, ened Composite Panels. — Ahmed K. Noor, in Complex Viscoelastoplastic and Damage Duane M. Revilock, Wieslaw K. Binienda, James H. Starnes, Jr., and Jeanne M. Peters; Modeling for Isotropic/Anisotropic Aerospace Walter Z. Nie, S. Ben Mackenzie, and Kevin B. 15(4), 154-64 (2002). Materials. — A. F. Saleeb, T. E. Wilt, D. A. Todd; 15(3), 104-10 (2002). Todd, Kevin B. Trowbridge, and A. S. Gendy; 15(3), 84-96 Saad, Ahmed A. Impact Testing and Analysis of Composites for Air- (2002). Fluid Mechanism of Wing Rock for Configurations craft Engine Fan Cases. — Gary D. Roberts, Errata for “Effective Strategy for Automated Char- with Chine-Shaped Forebodies. — Ahmed A. Duane M. Revilock, Wieslaw K. Binienda, acterization in Complex Viscoelastoplastic and Saad, Brad S. Liebst, and Raymond E. Gordnier; Walter Z. Nie, S. Ben Mackenzie, and Kevin B. 15(4), 125-35 (2002). Todd; 15(3), 104-10 (2002). Damage Modeling for Isotropic/Anisotropic Aerospace Materials” by A. F. Saleeb, T. E. Wilt, Saleeb, A. F. Trowbridge, D. A. Effective Strategy for Automated Characterization Effective Strategy for Automated Characterization D. A. Trowbridge, and A. S. Gendy. — A. F. Sa- in Complex Viscoelastoplastic and Damage in Complex Viscoelastoplastic and Damage leeb, T. E. Wilt, D. A. Trowbridge, and A. S. Modeling for Isotropic/Anisotropic Aerospace Modeling for Isotropic/Anisotropic Aerospace Gendy; 15(4), 166 (2002). Materials. — A. F. Saleeb, T. E. Wilt, D. A. Materials. — A. F. Saleeb, T. E. Wilt, D. A. Yadav, Dayanand Trowbridge, and A. S. Gendy; 15(3), 84-96 Trowbridge, and A. S. Gendy; 15(3), 84-96 Stability of Curved Composite Panels with Ran- (2002). (2002). dom Material Properties. — Bhrigu N. Singh, N. Errata for “Effective Strategy for Automated Char- Errata for “‘Effective Strategy for Automated Char- acterization in Complex Viscoelastoplastic and acterization in Complex Viscoelastoplastic and G. R. Iyengar, and Dayanand Yadav; 15(2), Damage Modeling for Isotropic/Anisotropic Damage Modeling for Isotropic/Anisotropic 46-54 (2002). Aerospace Materials” by A. F. Saleeb, T. E. Wilt, Aerospace Materials” by A. F. Saleeb, T. E. Wilt, Yedavalli, Rama K. D. A. Trowbridge, and A. S. Gendy. — A. F. Sa- D. A. Trowbridge, and A. S. Gendy. — A. F. Sa- Acceleration Feedback-Based Active and Passive leeb, T. E. Wilt, D. A. Trowbridge, and A. S. leeb, T. E. Wilt, D. A. Trowbridge, and A. S. Vibration Control of Landing Gear Components. Gendy; 15(4), 166 (2002). Gendy; 15(4), 166 (2002). — Seung-Keon Kwak, Gregory Washington, Singh, Bhrigu N. Washington, Gregory and Rama K. Yedavalli; 15(1), 1-9 (2002). Stability of Curved Composite Panels with Ran- Acceleration Feedback-Based Active and Passive dom Material Properties. — Bhrigu N. Singh, N. Vibration Control of Landing Gear Components. Zou, G. P. G. R. Iyengar, and Dayanand Yadav; 15(2), — Seung-Keon Kwak, Gregory Washington, Active Vibration Damping of Composite Beam 46-54 (2002). and Rama K. Yedavalli; 15(1), 1-9 (2002). using Smart Sensors and Actuators. — G. Song, Song, G. Watson, W. P. Z. Qiao, W. K. Binienda, and G. P. Zou; 15(3), Active Vibration Damping of Composite Beam Integrity of Sandwich Panels and Beams with 97-103 (2002). using Smart Sensors and Actuators. — G. Song, Truss-Reinforced Cores. — C. Kocher, W. Wat- P. Z. Qiao, W. K. Binienda, and G. P. Zou; 15(3), son, M. Gomez, I. Gonzalez, and V. Birman; 97-103 (2002). 15(3), 111-7 (2002). 170 / JOURNAL OF AEROSPACE ENGINEERING / OCTOBER 2002