Journal of Aerospace Engineering 2008: Vol 21 Index & Table of Contents

2008·1.7 MB·English

Jingyun Cheng and Wieslaw K. Binienda; 21 (3), gence, and Control — Ye-Hwa Chen; 21 (4), nates under Prestress — D. Zheng and W. K.
152-61 (2008). 288-93 (2008). Binienda; 21 (4), 197-205 (2008).
Dust Fiber optics Quasi-Static Indentation Behavior of Honeycomb
Characterization of Lunar Dust for Toxicological Solar Thermal Power for Lunar Materials Sandwich Materials and Its Application in Im-
Studies. I: Particle Size Distribution — Jaesung Processing — Takashi Nakamura and Constance pact Simulations Mijia Yang and Pizhong
Park, Yang Liu, Kenneth D. Kihm, and L. Senior; 21 (2), 91-101 (2008). Qiao; 21 (4), 226-34 (2008).
Lawrence A. Taylor; 21 (4), 266-71 (2008). Fiber reinforced polymers Impact Mechanics and High-Energy Absorbing
Characterization of Lunar Dust for Toxicological Rate-Dependent Shell Element Composite Mate- Materials: Review — Pizhong Qiao, Mijia Yang,
Studies. II: Texture and Shape Characteristics — rial Model Implementation in LS-DYNA — Xi- and Florin Bobaru; 21 (4), 235-48 (2008).
Yang Liu, Jaesung Park, Darren Schnare, Eddy ahua Zheng and Wieslaw K. Binienda; 21 (3),
Assessment of Residual Tensile Strength of
Hill, and Lawrence A. Taylor; 21 (4), 272-9 140-51 (2008).
Carbon/Epoxy Composites Subjected to Low-
(2008). Full-Scale Testing and Analysis for Blast-Resistant
Energy Impact Ayman Mosallam, Joel Slenk,
Dynamics Design — Arup K. Maji, Jay P. Brown, and and Jesa Kreiner; 21 (4), 249-58 (2008).
Robust Stationkeeping Control for Libration Point Girum S. Urgessa; 21 (4), 217-25 (2008).
Quasi-Periodic Orbits — Yunjun Xu and Shan- Finite difference method Impact loads
kar Suman; 21 (2), 102-15 (2008). Impact Mechanics and High-Energy Absorbing Peridynamic Analysis of Impact Damage in Com-
posite Laminates Jifeng Xu, Abe Askari, Olaf
Mechanical Behavior of Metallic Hollow Sphere Materials: Review — Pizhong Qiao, Mijia Yang,
Weckner, and Stewart Silling; 21 (3), 187-94
Materials: Experimental Study — Z. Y. Gao, T. and Florin Bobaru; 21 (4), 235-48 (2008).
X. Yu, and H. Zhao; 21 (4), 206-16 (2008). Finite element method (2008).
Impact Mechanics and High-Energy Absorbing Model for the Force—Displacement Relationship of Kalman filters
Materials: Review — Pizhong Qiao, Mijia Yang, Wire Rope Springs — Rafik R. Gerges; 21 (1), Aircraft Icing Detection, Identification, and Recon
and Florin Bobaru; 21 (4), 235-48 (2008). 1-9 (2008). figurable Control Based on Kalman Filtering and
Energy Closed-Form Isoparametric Shape Functions of Neural Networks Fikret Caliskan, Rahmi
Closed-Form Isoparametric Shape Functions of Four-Node Convex Finite Elements Gautam Aykan, and Chingiz Hajiyev; 21 (2), 51-60
Four-Node Convex Finite Elements — Gautam Dasgupta; 21 (1), 10-8 (2008). (2008).
Dasgupta; 21 (1), 10-8 (2008). Stiffness Matrices of Isoparametric Four-Node Fi- Laminates
Energy Dissipation in Spacecraft Structures Incor- nite Elements by Exact Analytical Integration Failure Model for Rate-Dependent Polymer Matrix
porating Bolted Joints Operating in Macroslip Gautam Dasgupta; 21 (2), 45-50 (2008). Composite Laminates under High-Velocity
— R. Wang, A. D. Crocombe, G. Richardson, Simplified Braiding through Integration Points Impact — Linfa Zhu, Aditi Chattopadhyay, and
and C. I. Underwood; 21 (1), 19-26 (2008). Model for Triaxially Braided Composites Robert K. Goldberg; 21 (3), 132-9 (2008).
Energy absorption Jingyun Cheng and Wieslaw K. Binienda; 21 (3), Peridynamic Analysis of Impact Damage in Com-
Impact Mechanics and High-Energy Absorbing 152-61 (2008). posite Laminates Jifeng Xu, Abe Askari, Olaf
Materials: Review — Pizhong Qiao, Mijia Yang, Impact Mechanics and High-Energy Absorbing Weckner, and Stewart Silling; 21 (3), 187-94
and Florin Bobaru; 21 (4), 235-48 (2008). Materials: Review — Pizhong Qiao, Mijia Yang, (2008).
Engines and Florin Bobaru; 21 (4), 235-48 (2008). Analysis of Impact Response of Composite Lami-
Gouging and Fracture of Engine Containment Foam nates under Prestress D. Zheng and W. K.
Structure under Fragment Impact — X. Teng and Mechanical Behavior of Metallic Hollow Sphere Binienda; 21 (4), 197-205 (2008)
T. Wierzbicki; 21 (3), 174-86 (2008). Materials: Experimental Study — Z. Y. Gao, T.
Launching
Environmental issues X. Yu, and H. Zhao; 21 (4), 206-16 (2008). Energy Dissipation in Spacecraft Structures Incor
Technical Requirements for Lunar Structures Friction porating Bolted Joints Operating in Macroslip
Alexander M. Jablonski and Kelly A. Ogden; 21 Model for the Force—Displacement Relationship of R. Wang, A. D. Crocombe, G. Richardson,
(2), 72-90 (2008). Wire Rope Springs Rafik R. Gerges; 21 (1), and C. I. Underwood; 21 (1), 19-26 (2008)
Epoxy compounds 1-9 (2008).
Manufacturing
Assessment of Residual Tensile Strength of Full-scale tests
Solar Thermal Power for Lunar Materials
Carbon/Epoxy Composites Subjected to Low- Full-Scale Testing and Analysis for Blast-Resistant
Processing Takashi Nakamura and Constance
Energy Impact — Ayman Mosallam, Joel Slenk, Design Arup K. Maji, Jay P. Brown, and
L. Senior; 21 (2), 91-101 (2008)
and Jesa Kreiner; 21 (4), 249-58 (2008). Girum S. Urgessa; 21 (4), 217-25 (2008).
Epoxy resins Honeycomb structures Masonry
Measurement of Epoxy Resin Tension, Compres- Quasi-Static Indentation Behavior of Honeycomb Full-Scale Testing and Analysis for Blast-Resistant
sion, and Shear Stress—Strain Curves over a Sandwich Materials and Its Application in Im- Design Arup K. Maji, Jay P. Brown, and
Wide Range of Strain Rates Using Small Test pact Simulations Mijia Yang and Pizhong Girum S. Urgessa; 21 (4), 217-25 (2008)
Specimens Justin D. Littell, Charles R. Rug- Qiao; 21 (4), 226-34 (2008). Material properties
geri, Robert K. Goldberg, Gary D. Roberts, Wil- Impact Mechanics and High-Energy Absorbing Measurement of Epoxy Resin Tension, Compres-
liam A. Arnold, and Wieslaw K. Binienda; 21 Materials: Review Pizhong Qiao, Mijia Yang, sion, and Shear Stress—Strain Curves over a
(3), 162-73 (2008). and Florin Bobaru; 21 (4), 235-48 (2008) Wide Range of Strain Rates Using Small Test
Excavation Hysteresis Specimens Justin D. Littell, Charles R. Rug
Position Accommodation and Compliance Control Model for the Force—Displacement Relationship of geri, Robert K. Goldberg, Gary D. Roberts, Wil-
for Robotic Excavation — William Richardson- Wire Rope Springs — Rafik R. Gerges; 21 (1), liam A. Arnold, and Wieslaw K. Binienda; 21
Little and Christopher Damaren; 21 (1), 27-34 1-9 (2008). (3), 162-73 (2008)
(2008). Ice Material tests
Failure modes Aircraft Icing Detection, Identification, and Recon- Measurement of Epoxy Resin Tension, Compres-
Failure Model for Rate-Dependent Polymer Matrix figurable Control Based on Kalman Filtering and sion, and Shear Stress—Strain Curves over a
Composite Laminates under High-Velocity Neural Networks Fikret Caliskan, Rahmi Wide Range of Strain Rates Using Small Test
Impact — Linfa Zhu, Aditi Chattopadhyay, and Aykan, and Chingiz Hajiyev; 21 (2), 51-60 Specimens Justin D. Littell, Charles R. Rug-
Robert K. Goldberg; 21 (3), 132-9 (2008). (2008). geri, Robert K. Goldberg, Gary D. Roberts, Wil-
Feedback control Impact liam A. Arnold, and Wieslaw K. Binienda; 21
Artificial Swarm System: Boundedness, Conver- Analysis of Impact Response of Composite Lami- (3), 162-73 (2008).
JOURNAL OF AEROSPACE ENGINEERING © ASCE / OCTOBER 2008 / 295
Matrices, mathematics Oxygen Sandwich structures
Stiffness Matrices of Isoparametric Four-Node Fi- Solar Thermal Power for Lunar Materials Quasi-Static Indentation Behavior of Honeycomb
nite Elements by Exact Analytical Integration — Processing — Takashi Nakamura and Constance Sandwich Materials and Its Application in Im-
Gautam Dasgupta; 21 (2), 45-50 (2008). L. Senior; 21 (2), 91-101 (2008). pact Simulations — Mijia Yang and Pizhong
Measurement Parameters Qiao; 21 (4), 226-34 (2008).
Measurement of Epoxy Resin Tension, Compres- Closed-Form Isoparametric Shape Functions of Impact Mechanics and High-Energy Absorbing
sion, and Shear Stress—Strain Curves over a Four-Node Convex Finite Elements — Gautam Materials: Review Pizhong Qiao, Mijia Yang,
Wide Range of Strain Rates Using Small Test Dasgupta; 21 (1), 10-8 (2008). and Florin Bobaru; 21 (4), 235-48 (2008).
Specimens — Justin D. Littell, Charles R. Rug- Particle size Satellites
geri, Robert K. Goldberg, Gary D. Roberts, Wil- Characterization of Lunar Dust for Toxicological Robust Stationkeeping Control for Libration Point
liam A. Arnold, and Wieslaw K. Binienda; 21 Studies. I: Particle Size Distribution — Jaesung Quasi-Periodic Orbits — Yunjun Xu and Shan-
(3), 162-73 (2008) Park, Yang Liu, Kenneth D. Kihm, and kar Suman; 21 (2), 102-15 (2008).
Mechanical systems Lawrence A. Taylor; 21 (4), 266-71 (2008)
Seismic design
Artificial Swarm System: Boundedness, Conver Passive control Model for the Force—Displacement Relationship of
gence, and Control Ye-Hwa Chen; 21 (4), Model for the Force—Displacement Relationship of Wire Rope Springs — Rafik R. Gerges; 21 (1),
288-93 (2008). Wire Rope Springs — Rafik R. Gerges; 21 (1), 1-9 (2008).
Models 1-9 (2008)
Sensors
Full-Scale Testing and Analysis for Blast-Resistant Plasticity Three-Dimensional Electromechanical Impedance
GDiesriugmn S. UrgAersuspa K. 21 Ma(j4)i, ,, 22J11a77y - 25P . (B2r0o0w8n)., and FeasBirbiidligtey Iomfp aTchte rmProoptleacsttiiocn Co— mNpaossiimt e UdJdaicnk,e tsJ ohfonr SMtordueclt urfeo r MIuntletriapcltei onP iezoceVreanmui c GTorpaaln sdMuacdehrasv—
Moon D. Purdue, and Uday Vaidya; 21 (4), 259-65 Annamdas and Chee Kiong Soh; 21 (1), 35-44
Technical Requirements for Lunar Structures (2008). (2008).
Alexander M. Jablonski and Kelly A. Ogden; 21 Plates
(2y) . 72-90 (2008 Simplified Braiding through Integration Points Shape
Closed-Form Isoparametric Shape Functions of
Solar Thermal Power for Lunar Materials Model for Triaxially Braided Composites —
Four-Node Convex Finite Elements — Gautam
Processing — Takashi Nakamura and Constance Jingyun Cheng and Wieslaw K. Binienda; 21 (3),
Dasgupta; 21 (1), 10-8 (2008).
L. Senior; 21 (2), 91-101 (2008). 152-61 (2008).
Shells
Characterization of Lunar Dust for Toxicological Polymers
Rate-Dependent Shell Element Composite Mate-
Studies. I: Particle Size Distribution — Jaesung Approximation of Nonlinear Unloading Effects in
rial Model Implementation in LS-DYNA — Xi-
Park, Yang Liu, Kenneth D. Kihm, and the Strain Rate Dependent Deformation Analy-
ahua Zheng and Wieslaw K. Binienda; 21 (3),
Lawrence A. Taylor; 21 (4), 266-71 (2008). sis of Polymer Matrix Materials Utilizing a State
140-51 (2008).
Characterization of Lunar Dust for Toxicological Variable Approach Robert K. Goldberg, Gary
Studies. II: Texture and Shape Characteristics D. Roberts, Justin D. Littell, and Wieslaw K Shock waves
Yang Liu, Jaesung Park, Darren Schnare, Eddy Binienda; 21 (3), 119-31 (2008) Impact Mechanics and High-Energy Absorbing
Hill, and Lawrence A. Taylor; 21 (4), 5792 72-9 Failure Model for Rate-Dependent Polymer Matrix Materials: Review — Pizhong Qiao, Mijia Yang,
(2008). Composite Laminates under High-Velocity and Florin Bobaru; 21 (4), 235-48 (2008).
Morphology Impact — Linfa Zhu, Aditi Chattopadhyay, and Simulation
Characterization of Lunar Dust for Toxicological Robert K. Goldberg; 21 (3), 132-9 (2008). Quasi-Static Indentation Behavior of Honeycomb
Studies. II: Texture and Shape Characteristics Simplified Braiding through Integration Points Sandwich Materials and Its Application in Im-
Yang Liu, Jaesung Park, Darren Schnare, Eddy Model for Triaxially Braided Composites pact Simulations Mijia Yang and Pizhong
Hill, and Lawrence A. Taylor; 21 (4), 272-9 Jingyun Cheng and Wieslaw K. Binienda; 21 (3), Qiao; 21 (4), 226-34 (2008).
(2008) 152-61 (2008) Size effect
Neural networks easurement of Epoxy Resin Tension, Compres- Gouging and Fracture of Engine Containment
Aircraft Icing Detection, Identification, and Recon- sion, and Shear Stress—Strain Curves over a Structure under Fragment Impact — X. Teng and
figurable Control Based on Kalman Filtering and Wide Range of Strain Rates Using Small Test I. Wierzbicki; 21 (3), 174-86 (2008).
Neural Networks Fikret Caliskan, Rahmi Specimens Justin D. Littell, Charles R. Rug- Slip
Aykan, and Chingiz Hajiyev; 21 (2), 51-60 geri, Robert K. Goldberg, Gary D. Roberts, Wil- Energy Dissipation in Spacecraft Structures Incor-
(2008) liam A. Arnold, and Wieslaw K. Binienda; 21
porating Bolted Joints Operating in Macroslip
Noise control (3), 162-73 (2008). R. Wang, A. D. Crocombe, G. Richardson,
Ihree-Dimensional Electromechanical Impedance Prestressing and C. I. Underwood; 21 (1), 19-26 (2008)
Model for Multiple Piezoceramic Transducers Analysis of Impact Response of Composite Lami-
Solar energy
Structure Interaction Venu Gopal Madhav nates under Prestress D. Zheng and W. K.
Solar Thermal Power for Lunar Materials
Annamdas and Chee Kiong Soh; 21 (1), 35-44 Binienda; 21 (4), 197-205 (2008).
Processing — Takashi Nakamura and Constance
(2008). Protective structures L. Senior; 21 (2), 91-101 (2008).
Nondestructive tests Feasibility of Thermoplastic Composite Jackets for
Space colonies
Three-Dimensional Electromechanical Impedance Bridge Impact Protection — Nasim Uddin, John
Technical Requirements for Lunar Structures
Model for Multiple Piezoceramic Transducers D. Purdue, and Uday Vaidya; 21 (4), 259-65
Alexander M. Jablonski and Kelly A. Ogden; 21
Structure Interaction Venu Gopal Madhav (2008).
(2), 72-90 (2008)
Annamdas and Chee Kiong Soh; 21 (1), 35-44 Residual strength
(2008). Assessment of Residual Tensile Strength of Solar Thermal Power for Lunar Materials
Nonlinear analysis Carbon/Epoxy Composites Subjected to Low- Processing — Takashi Nakaamnd uConrstaanc e
L. Senior; 21 (2), 91-101 (2008).
Artificial Swarm System: Boundedness, Conver- Energy Impact Ayman Mosallam, Joel Slenk,
gence, and Control Ye-Hwa Chen; 21 (4), and Jesa Kreiner; 21 (4), 249-58 (2008). Space construction
288-93 (2008) Robotics Technical Requirements for Lunar Structures
Nonlinear methods Position Accommodation and Compliance Control Alexander M. Jablonski and Kelly A. Ogden; 21
Impact Mechanics and High-Energy Absorbing for Robotic Excavation — William Richardson- (2), 72-90 (2008).
Materials: Review — Pizhong Qiao, Mijia Yang, Little and Christopher Damaren; 21 (1), 27-34 Space exploration
and Florin Bobaru; 21 (4), 235-48 (2008). (2008). Technical Requirements for Lunar Structures —
296 / JOURNAL OF AEROSPACE ENGINEERING © ASCE / OCTOBER 2008
Alexander M. Jablonski and Kelly A. Ogden; 21 liam A. Arnold, and Wieslaw K. Binienda; 21 Yang Liu, Jaesung Park, Darren Schnare, Eddy
(2), 72-90 (2008). (3). 162-73 (2008). Hill, and Lawrence A. Taylor; 21 (4), 272-9
Solar Thermal Power for Lunar Materials Impact Mechanics and High-Energy Absorbing (2008)
Processing — Takashi Nakamura and Constance Materials: Review Pizhong Qiao, Mijia Yang, Turbulent flow
L. Senior; 21 (2), 91-101 (2008). and Florin Bobaru; 21 (4), 235-48 (2008) Wind Environmental Conditions in Passages be-
Space shuttle orbiter Structural analysis tween Two Long Narrow Perper
Robust Stationkeeping Control for Libration Point Energy Dissipation in Spacecraft Structures Incor Buildings — B. Blocken, T. Stathopoulos, and J
Quasi-Periodic Orbits Yunjun Xu and Shan- porating Bolted Joints Operating in Macroslip Carmeliet; 21 (4), 280-7 (2008)
kar Suman; 21 (2), 102-15 (2008). R. Wang, A. D. Crocombe, G. Richardson, Velocity
Space structures and C. I. Underwood; 21 (1), 19-26 (2008) Failure Model for Rate-Dependent Polymer Matrix
Coupling among Pitch Motion, Axial Vibration, Structural dynamics Composite Laminates under Hig
and Orbital Motion of Large Space Structures Coupling among Pitch Motion, Axial Vibration, Impact Linfa Zhu, Aditi Chat
Kosei Ishimura and Ken Higuchi; 21 (2), 61-71 and Orbital Motion of Large Space Structures Robert K. Goldberg; 21 (3), 13
(2008). Kosei Ishimura and Ken Higuchi; 21 (2), 61- Vibration
Technical Requirements for Lunar Structures (2008). Model for the Force—Displacement Relationship
Alexander M. Jablonski and Kelly A. Ogden; 21 Temperature effects Wire Rope Springs Rafik R. Gerges: 21
(2), 72-90 (2008). Measurement of Epoxy Resin Tension, Compres- 1-9 (2008
Spacecraft sion, and Shear Stress—Strain Curves over a Three-Dimensional Electrome
Energy Dissipation in Spacecraft Structures Incor- Wide Range of Strain Rates Using Small Test Model for Multiple Piezoceramic Tr
porating Bolted Joints Operating in Macroslip Specimens Justin D. Littell, Charles R. Rug- Structure Interaction Venu Gop:
— R. Wang, A. D. Crocombe, G. Richardson, geri, Robert K. Goldberg, Gary D. Roberts, Wil Annamdas and Chee Kiong Sol
and C. I. Underwood; 21 (1), 19-26 (2008). liam A. Arnold, and Wieslaw K. Binienda; 21 (2008)
Spheres 162- 3 (2008). Coupling amon
Mechanical Behavior of Metallic Hollow Sphere Tensile strength ind Orbita
Kosei Ishi
Materials: Experimental Study Z. Y. Gao, T Assessment of Residual Tensile Strength of
X. Yu, and H. Zhao; 21 (4), 206-16 (2008) Carbon/Epoxy Composites Subjected to Low (2008)
Stability Energy Impact Ayman Mosallam, Joel Slenk, Viscoplasticity
Artificial Swarm System: Boundedness, Conver- and Jesa Kreiner; 21 (44) 249-58 (2008)
gence, and Control Ye-Hwa Chen; 21 (4), Thermal energy
288-93 (2008) Solar Thermal Power for Lunar Materials
Stiffness Processing — Takashi Nakamura and Constance
Stiffness Matrices of Isoparametric Four-Node Fi L. Senior; 21 (2), 91-101 (2008
Bini *nda
nite Elements by Exact Analytical Integration Thermal factors
Wind
Gautam Dasgupta; 21 (2~) , 45-50 (2008) Feasibility of Thermoplastic Composite Jackets for
Mode
Strain rate Bridge Impact Protection Nasim Uddin, John
Approximation of Nonlinear Unloading Effects in D. Purdue, and Uday Vaidya; 21 (4), 259-65 9 (2008
the Strain Rate Dependent Deformation Analy- (2008) Wind speed
sis of Polymer Matrix Materials Utilizing a State Three-dimensional models
Variable Approach — Robert K. Goldberg, Gary Three-Dimensional Electromechanical Impedance
D. Roberts, Justin D. Littell, and Wieslaw K Model for Multiple Piezoceramic Transducers
Binienda; 21 (3), 119-31 (2008). Structure Interactior \ Gopal Madhav
Rate-Dependent Shell Element Composite Mate Annamdas and Chee Kiong Soh; 21 35-44
rial Model Implementation in LS-DYNA — Xi (2008)
ahua Zheng and Wieslaw K. Binienda; 21 (3 Toxicity
140-51 (2008).
Measurement of Epoxy Resin Tension, Compres-
sion, and Shear Stress—Strain Curves over a
Wide Range of Strain Rates Using Small Test
Specimens Justin D. Littell, Charles R. Rug
geri, Robert K. Goldberg, Gary D. Roberts, Wil Studies. Il: Texture an
JOURNAL OF AEROSPACE ENGINEERING © ASCE / OCTOBER 2008 / 297
2008 ANNUAL INDEX
Author Index
Annamdas, Venu Gopal Madhav Buildings — B. BlockenT,. Stathopoulos, and J. Wire Rope Springs - Rafik R. Gerges; 21 (1),
Three-Dimensional Electromechanical Impedance Carmeliet; 21 (4), 280-7 (2008). 1-9 (2008).
Model for Multiple Piezoceramic Transducers— Bobaru, Florin Goldberg, Robert K.
Structure Interaction Venu Gopal Madhav Impact Mechanics and High-Energy Absorbing Approximation of Nonlinear Unloading Effects in
Annamdas and Chee Kieng Soh; 21 (1), 35-44 Materials: Review — Pizhong Qiao, Mijia Yang, the Strain Rate Dependent Deformation Analy-
(2008). and Florin Bobaru; 21 (4), 235-48 (2008). sis of Polymer Matrix Materials Utilizing a State
Arnold, William A. Brown, Jay P. Variable Approach — Robert K. Goldberg, Gary
Measurement of Epoxy Resin Tension, Compres- Full-Scale Testing and Analysis for Blast-Resistant D. Roberts, Justin D. Littell, and Wieslaw K.
sion, and Shear Stress—Strain Curves over a Design — Arup K. Maji, Jay P. Brown, and Binienda; 21 (3), 119-31 (2008).
Wide Range of Strain Rates Using Small Test Girum S. Urgessa; 21 (4), 217-25 (2008). Failure Model for Rate-Dependent Polymer Matrix
Specimens — Justin D. Littell, Charles R. Rug- Caliskan, Fikret Composite Laminates under High-Velocity
geri, Robert K. Goldberg, Gary D. Roberts, Wil- Aircraft Icing Detection, Identification, and Recon- Impact — Linfa Zhu, Aditi Chattopadhyay, and
liam A. Arnold, and Wieslaw K. Binienda; 21 figurable Control Based on Kalman Filtering and Robert K. Goldberg; 21 (3), 132-9 (2008).
(3), 162-73 (2008) Neural Networks Fikret Caliskan, Rahmi Measurement of Epoxy Resin Tension, Compres-
Askari, Abe Aykan, and Chingiz Hajiyev; 21 (2), 51-60
sion, and Shear Stress—Strain Curves over a
Peridynamic Analysis of Impact Damage in Com- (2008).
Wide Range of Strain Rates Using Small Test
posite Laminates Jifeng Xu, Abe Askari, Olaf Carmeliet, J. Specimens — Justin D. Littell, Charles R. Rug-
Weckner, and Stewart Silling; 21 (3), 187-94 Wind Environmental Conditions in Passages be- geri, Robert K. Goldberg, Gary D. Roberts, Wil-
(2008). tween Two Long Narrow Perpendicular liam A. Arnold, and Wieslaw K. Binienda; 21
Aykan, Rahmi Buildings — B. BlockenT,. Stathopoulos, and J.
(3), 162-73 (2008).
Aircraft Icing Detection, Identification, and Recon- Carmeliet; 21 (4), 280-7 (2008).
figurable Control Based on Kalman Filtering and Chattopadhyay, Aditi Hajiyev, Chingiz
Neural Networks Fikret Caliskan, Rahmi Failure Model for Rate-Dependent Polymer Matrix Aircraft Icing Detection, Identification, and Recon-
Aykan, and Chingiz Hajiyev; 21 (2), 51-60 Composite Laminates under High-Velocity figurable Control Based on Kalman Filtering and
(2008). Impact — Linfa Zhu, Aditi Chattopadhyay, and Neural Networks Fikret Caliskan, Rahmi
Binienda, Wieslaw K. Robert K. Goldberg; 21 (3), 132-9 (2008). Aykan, and Chingiz Hajiyev; 21 (2), 51-60
Impact Mechanics of Composite Materials for Chen, Ye-Hwa (2008).
Aerospace Application Pizhong Qiao and Artificial Swarm System: Boundedness, Conver- Higuchi, Ken
Wieslaw K. Binienda; 21 (3), 117-8 (2008). gence, and Control — Ye-Hwa Chen; 21 (4), Coupling among Pitch Motion, Axial Vibration,
Approximation of Nonlinear Unloading Effects in 288-93 (2008). and Orbital Motion of Large Space Structures —
the Strain Rate Dependent Deformation Analy- Cheng, Jingyun Kosei Ishimura and Ken Higuchi; 21 (2), 61-71
sis of Polymer Matrix Materials Utilizing a State Simplified Braiding through Integration Points (2008).
Variable Approach — Robert K. Goldberg, Gary
Model for Triaxially Braided Composites Hill, Eddy
D. Roberts, Justin D. Littell, and Wieslaw K.
Jingyun Cheng and Wieslaw K. Binienda; 21 (3), Characterization of Lunar Dust for Toxicological
Binienda; 21 (3), 119-31 (2008)
152-61 (2008). Studies. II: Texture and Shape Characteristics —
Rate-Dependent Shell Element Composite Mate-
Crocombe, A. D. Yang Liu, Jaesung Park, Darren Schnare, Eddy
rial Model Implementation in LS-DYNA — Xi-
Energy Dissipation in Spacecraft Structures Incor- Hill, and Lawrence A. Taylor; 21 (4), 272-9
ahua Zheng and Wieslaw K. Binienda; 21 (3),
140-51 (2008) porating Bolted Joints Operating in Macroslip (2008).
Simplified Braiding through Integration Points R. Wang, A. D. Crocombe, G. Richardson, Ishimura, Kosei
Model for Triaxially Braided Composites and C. I. Underwood; 21 (1), 19-26 (2008). Coupling among Pitch Motion, Axial Vibration,
Jingyun Cheng and Wieslaw K. Binienda; 21 (3), Damaren, Christopher and Orbital Motion of Large Space Structures —
152-61 (2008). Position Accommodation and Compliance Control Kosei Ishimura and Ken Higuchi; 21 (2), 61-71
Measurement of Epoxy Resin Tension, Compres- for Robotic Excavation — William Richardson- (2008).
sion, and Shear Stress—Strain Curves over a Little and Christopher Damaren; 21 (1), 27-34 Jablonski, Alexander M.
Wide Range of Strain Rates Using Small Test (2008). Technical Requirements for Lunar Structures —
Specimens — Justin D. Littell, Charles R. Rug- Dasgupta, Gautam
Alexander M. Jablonski and Kelly A. Ogden; 21
geri, Robert K. Goldberg, Gary D. Roberts, Wil- Closed-Form Isoparametric Shape Functions of
(2), 72-90 (2008).
liam A. Arnold, and Wieslaw K. Binienda; 21 Four-Node Convex Finite Elements — Gautam
(3), 162-73 (2008). Dasgupta; 21 (1), 10-8 (2008). Kihm, Kenneth D.
Impact Behavior and High-Energy Absorbing Stiffness Matrices of Isoparametric Four-Node Fi- Characterization of Lunar Dust for Toxicological
Materials — Pizhong Qiao and Wieslaw K. nite Elements by Exact Analytical Integration — Studies. I: Particle Size Distribution — Jaesung
Binienda; 21 (4), 195-6 (2008). Gautam Dasgupta; 21 (2), 45-50 (2008). Park, Yang Liu, Kenneth D. Kihm, and
Analysis of Impact Response of Composite Lami- Gao, Z. Y. Lawrence A. Taylor; 21 (4), 266-71 (2008).
nates under Prestress D. Zheng and W. K. Mechanical Behavior of Metallic Hollow Sphere Kreiner, Jesa
Binienda; 21 (4), 197-205 (2008). Materials: Experimental Study — Z. Y. Gao, T. Assessment of Residual Tensile Strength of
Blocken, B. X. Yu, and H. Zhao; 21 (4), 206-16 (2008). Carbon/Epoxy Composites Subjected to Low-
Wind Environmental Conditions in Passages be- Gerges, Rafik R. Energy Impact — Ayman Mosallam, Joel Slenk,
tween Two Long Narrow Perpendicular Model for the Force—Displacement Relationship of and Jesa Kreiner; 21 (4), 249-58 (2008).
298 / JOURNAL OF AEROSPACE ENGINEERING © ASCE / OCTOBER 2008
Littell, Justin D. and Florin Bobaru; 21 (4), 235-48 (2008). Taylor, Lawrence A.
Approximation of Nonlinear Unloading Effects in Richardson, G. Characterization of Lunar Dust for Toxicological
the Strain Rate Dependent Deformation Analy- Energy Dissipation in Spacecraft Structures Incor- Studies. I: Particle Size Distribution — Jaesung
sis of Polymer Matrix Materials Utilizing a State porating Bolted Joints Operating in Macroslip Park, Yang Liu, Kenneth D. Kihm, and
Variable Approach — Robert K. Goldberg, Gary — R. Wang, A. D. Crocombe, G. Richardson, Lawrence A. Taylor; 21 (4), 266-71 (2008)
D. Roberts, Justin D. Littell, and Wieslaw K. and C. I. Underwood; 21 (1), 19-26 (2008). Characterization of Lunar Dust for Toxicological
Binienda; 21 (3), 119-31 (2008). Richardson-Little, William Studies. II: Texture and Shape Characteristics
Measurement of Epoxy Resin Tension, Compres- Position Accommodation and Compliance Control Yang Liu, Jaesung Park, Darren Schnare, Eddy
sion, and Shear Stress—Strain Curves over a for Robotic Excavation — William Richardson- Hill, and Lawrence A. Taylor; 21 (4), 272-9
Wide Range of Strain Rates Using Small Test Little and Christopher Damaren; 21 (1), 27-34 (2008)
Specimens — Justin D. Littell, Charles R. Rug- (2008) Teng, X.
geri, Robert K. Goldberg, Gary D. Roberts, Wil- Roberts, Gary D. Gouging and Fracture of Engine Containment
liam A. Arnold, and Wieslaw K. Binienda; 21 Approximation of Nonlinear Unloading Effects in Structure under Fragment Impact X. Teng and
(3), 162-73 (2008).
the Strain Rate Dependent Deformation Analy- T. Wierzbicki; 21 (3), 174-86 (2008)
Liu, Yang sis of Polymer Matrix Materials Utilizing a State Uddin, Nasim
Characterization of Lunar Dust for Toxicological Variable Approach — Robert K. Goldberg, Gary Feasibility of Thermoplastic Composite Jackets for
Studies. I: Particle Size Distribution — Jaesung
D. Roberts, Justin D. Littell, and Wieslaw K Bridge Impact Protection — Nasim Uddin, John
Park, Yang Liu, Kenneth D. Kihm, and Binienda; 21 (3), 119-31 (2008). D. Purdue, and Uday Vaidya; 21 (4), 259-65
Lawrence A. Taylor; 21 (4), 266-71 (2008).
Measurement of Epoxy Resin Tension, Compres- (2008)
Characterization of Lunar Dust for Toxicological
sion, and Shear Stress—Strain Curves over a Underwood, C. I.
Studies. II: Texture and Shape Characteristics —
Wide Range of Strain Rates Using Small Test Energy Dissipation in Spacecraft Structures Incor-
Yang Liu, Jaesung Park, Darren Schnare, Eddy
Specimens — Justin D. Littell, Charles R. Rug- porating Bolted Joints Operating in Macroslip
Hill, and Lawrence A. Taylor; 21 (4), 272-9
geri, Robert K. Goldberg, Gary D. Roberts, Wil- R. Wang, A. D. Crocombe, G. Richardson,
(2008).
liam A. Arnold, and Wieslaw K. Binienda; 21 and C. I. Underwood; 21 (1), 19-26 (2008)
Maji, Arup K. (3), 162-73 (2008) Urgessa, Girum S.
Full-Scale Testing and Analysis for Blast-Resistant
Ruggeri, Charles R. Full-Scale Testing and Analysis for Blast-Resistant
Design — Arup K. Maji, Jay P. Brown, and
Measurement of Epoxy Resin Tension, Compres- Design Arup K. Maji, Jay P. Brown, and
Girum S. Urgessa; 21 (4), 217-25 (2008).
sion, and Shear Stress—Strain Curves over a Girum S. Urgessa; 21 (4), 217-25 (2008)
Mosallam, Ayman
Wide Range of Strain Rates Using Small Test Vaidya, Uday
Assessment of Residual Tensile Strength of
Specimens — Justin D. Littell, Charles R. Rug- Feasibility of Thermoplastic Composite Jackets for
Carbon/Epoxy Composites Subjected to Low-
Energy Impact — Ayman Mosallam, Joel Slenk, geri, Robert K. Goldberg, Gary D. Roberts, Wil- Bridge Impact Protection Nasim Uddin, John
liam A. Arnold, and Wieslaw K. Binienda; 21 D. Purdue, and Uday Vaidya; 21 (4), 259-65
and Jesa Kreiner; 21 (4), 249-58 (2008).
(3). 162-73 (2008) (2008)
Nakamura, Takashi
Schnare, Darren Wang, R.
Solar Thermal Power for Lunar Materials
Characterization of Lunar Dust for Toxicological Energy Dissipation in Spacecraft Structures Incor
Processing — Takashi Nakamura and Constance
Studies. II: Texture and Shape Characteristics - porating Bolted Joints Operating in Macroslip
L. Senior; 21 (2), 91-101 (2008).
Yang Liu, Jaesung Park, Darren Schnare, Eddy R. Wang, A. D. Crocombe, G. Richardson,
Ogden, Kelly A. Hill, and Lawrence A. Taylor; 21 (4), 272-9 and C. I. Underwood; 21 (1), 19-26 (2008)
Technical Requirements for Lunar Structures — (2008) Weckner, Olaf
Alexander M. Jablonski and Kelly A. Ogden; 21
(2), 72-90 (2008). Senior, Constance L. Peridynamic Analysis of Impact Damage in Com-
Solar Thermal Power for Lunar Materials posite Laminates Jifeng Xu, Abe Askari, Olaf
Park, Jaesung
Processing — Takashi Nakamura and Constance Weckner, and Stewart Silling; 21 (3), 187-94
Characterization of Lunar Dust for Toxicological
L. Senior; 21 (2), 91-101 (2008) (2008).
Studies. I: Particle Size Distribution — Jaesung
Silling, Stewart Wierzbicki, T.
Park, Yang Liu, Kenneth D. Kihm, and
Peridynamic Analysis of Impact Damage in Com- Gouging and Fracture of Engine Containment
Lawrence A. Taylor; 21 (4), 266-71 (2008).
posite Laminates Jifeng Xu, Abe Askari, Olaf Structure under Fragment Impact X. Teng and
Characterization of Lunar Dust for Toxicological
Weckner, and Stewart Silling; 21 (3), 187-94 T. Wierzbicki; 21 (3), 174-86 (2008)
Studies. II: Texture and Shape Characteristics -
Yang Liu, Jaesung Park, Darren Schnare, Eddy (2008) Xu, Jifeng
Hill, and Lawrence A. Taylor; 21 (4), 272-9 Slenk, Joel Peridynamic Analysis of Impact Damage in Com-
(2008). Assessment of Residual Tensile Strength of posite Laminates Jifeng Xu, Abe Askari, Olaf
Purdue, John D. Carbon/Epoxy Composites Subjected to Low- Weckner, and Stewart Silling; 21 (3), 187-94
Feasibility of Thermoplastic Composite Jackets for Energy Impact — Ayman Mosallam, Joel Slenk, (2008)
Bridge Impact Protection — Nasim Uddin, John and Jesa Kreiner; 21 (4), 249-58 (2008) Xu, Yunjun
D. Purdue, and Uday Vaidya; 21 (4), 259-65 Soh, Chee Kiong Robust Stationkeeping Control for Libration Point
(2008). Three-Dimensional Electromechanical Impedance Quasi-Periodic Orbits Yunjun Xu and Shan
Model for Multiple Piezoceramic Transducers kar Suman; 21 (2), 102-15 (2008)
Qiao, Pizhong
Impact Mechanics of Composite Materials for Structure Interaction — Venu Gopal Madhav Yang, Mijia
Aerospace Application — Pizhong Qiao and Annamdas and Chee Kiong Soh; 21 (1), 35-44 Quasi-Static Indentation Behavior of Honeycomb
Wieslaw K. Binienda; 21 (3), 117-8 (2008). (2008). Sandwich Materials and Its Application in Im-
Impact Behavior and High-Energy Absorbing Stathopoulos, T. pact Simulations Mijia Yang and Pizhong
Materials — Pizhong Qiao and Wieslaw K. Wind Environmental Conditions in Passages be- Qiao; 21 (4), 226-34 (2008).
Binienda; 21 (4), 195-6 (2008). tween Two Long Narrow Perpendicular Impact Mechanics and High-Energy Absorbing
Quasi-Static Indentation Behavior of Honeycomb Buildings — B. Blocken, T. Stathopoulos, and J. Materials: Review — Pizhong Qiao, Mijia Yang,
Sandwich Materials and Its Application in Im- Carmeliet; 21 (4), 280-7 (2008). and Florin Bobaru; 21 (4), 235-48 (2008)
pact Simulations — Mijia Yang and Pizhong Suman, Shankar Yu, T. X.
Qiao; 21 (4), 226-34 (2008). Robust Stationkeeping Control for Libration Point Mechanical Behavior of Metallic Hollow Sphere
Impact Mechanics and High-Energy Absorbing Quasi-Periodic Orbits — Yunjun Xu and Shan- Materials: Experimental Study — Z. Y. Gao, T.
Materials: Review — Pizhong Qiao, Mijia Yang, kar Suman; 21 (2), 102-15 (2008). X. Yu, and H. Zhao; 21 (4), 206-16 (2008).
JOURNAL OF AEROSPACE ENGINEERING © ASCE / OCTOBER 2008 / 299
Zhao, H. Binienda; 21 (4), 197-205 (2008). Zhu, Linfa
Mechanical Behavior of Metallic Hollow Sphere Zheng, Xiahua Failure Model for Rate-Dependent Polymer Matrix
Materials: Experimental Study — Z. Y. Gao, T. Rate-Dependent Shell Element Composite Mate- Composite Laminates under High-Velocity
X. Yu, and H. Zhao; 21 (4), 206-16 (2008). rial Model Implementation in LS-DYNA — Xi- Impact — Linfa Zhu, Aditi Chattopadhyay, and
Zheng, D. ahua Zheng and Wieslaw K. Binienda; 21 (3), Robert K. Goldberg; 21 (3), 132-9 (2008).
Analysis of Impact Response of Composite Lami-
140-51 (2008).
nates under Prestress D. Zheng and W. K.
300 / JOURNAL OF AEROSPACE ENGINEERING © ASCE / OCTOBER 2008