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Dade Huang
Dade Huang
Director of Software Development, AlphaSTAR Corporation
Verified email at alphastarcorp.com
Title
Cited by
Cited by
Year
Micromechanics-based progressive failure analysis prediction for WWFE-III composite coupon test cases
CC Chamis, F Abdi, M Garg, L Minnetyan, H Baid, D Huang, J Housner, ...
Journal of Composite Materials 47 (20-21), 2695-2712, 2013
1062013
Damage-tolerant composite design principles for aircraft components under fatigue service loading using multi-scale progressive failure analysis
S DorMohammdi, C Godines, F Abdi, D Huang, M Repupilli, L Minnetyan
Journal of Composite Materials 51 (15), 2181-2202, 2017
252017
Damage tolerant composite design principles for aircraft components under static service loading using multi-scale progressive failure analysis
C Godines, S DorMohammadi, F Abdi, M Villa Montero, D Huang, ...
Journal of Composite Materials 51 (10), 1393-1419, 2017
232017
Damage progression in carbon-fiber reinforced plastic I-beams
D Huang, L Minnetyan
Journal of Composites for Construction 2 (1), 38-45, 1998
201998
Cohesive zone model for surface cracks using finite element analysis
D Xie, M Garg, D Huang, F Abdi
49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2008
172008
Certification modeling of composites fuselage, considering effect of defects from fiber placement manufacturing processes
F Abdi, Z Gürdal, D Huang
55th AIAA Aerospace Sciences Meeting, 0691, 2017
162017
Predicting failure design envelop for composite material system using finite element and progressive failure analysis approach
M Garg, GH Abumeri, D Huang
Proceedings of the 52nd International SAMPE Symposium: Material and Process …, 2008
162008
Grain boundary engineering of new additive manufactured polycrystalline alloys
F Abdi, A Eftekharian, D Huang, RB Rebak, M Rahmane, ...
Forces in Mechanics 4, 100033, 2021
152021
Progressive fracture of stitched stiffened composite shear panels in the postbuckling range
D Huang, L Minnetyan
Journal of reinforced plastics and composites 20 (18), 1617-1632, 2001
102001
Validation of class of applications using progressive failure and discrete cohesive zone model for line and surface cracks
M Garg, G Abumeri, D Huang
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2009
92009
Comparison of failure mechanisms in composite structure
D Huang, F Abdi, R Ragalini, A Mosallam
INTERNATIONAL SAMPE SYMPOSIUM AND EXHIBITION, 418-432, 2003
92003
Simulation of crushing process in composite tubes
A Najafi, D Huang, M Rais-Rohani, F Abdi
51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2010
72010
3D print-material and process model and effect of defects on part performance
C Godines, S DorMohammdi, F Abdi, D Huang, I Roche Rios
Proceedings of the Science in the Age of Experience Simulia User Conference …, 2018
52018
Virtual testing of the X37 space vehicle
F Abdi, T Castillo, D Huang, V Chen, A Delmondo
INTERNATIONAL SAMPE SYMPOSIUM AND EXHIBITION, 1298-1306, 2002
52002
Progressive Failure Analysis (PFA) and Verification of Composite Test Panel Under Impact and Tension After Impact (TAI) Loading Using GENOA
D Huang, F Abdi, M Khatiblou
Contract No. FW809FAH, 1999
51999
Probabilistic cyclic fatigue of composite structures
L Minnetyan, C Chamis, F Abdi, D Huang
19th AIAA Applied Aerodynamics Conference, 1375, 2001
42001
Probabilistic Assessment of Fracture Progression in Composite Structures
CC Chamis, L Minnetyan, B Mauget, D Huang, F Addi
1998 Aircraft Structural Integrity Program Conference, 1999
41999
Cyclic fatigue of composite airfoil structures
L Minnetyan, D Huang, C Chamis, F Abdi
39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 1998
41998
Computational simulation of damage propagation in three-dimensional woven composites
D Huang
Clarkson University, 1998
41998
Erosion Evaluation of Gas-Turbine Grade CMC’s at Room and Elevated Temperatures
A Eftekharian, RP Panakarajupally, GN Morscher, D Huang, F Abdi, ...
Turbo Expo: Power for Land, Sea, and Air 84997, V006T02A007, 2021
32021
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