Các bài viết có thể truy cập công khai - Rakesh K. KapaniaTìm hiểu thêm
Không có ở bất kỳ nơi nào: 34
Vibration and buckling analysis of curvilinearly stiffened plates using finite element method
P Shi, RK Kapania, CY Dong
Aiaa Journal 53 (5), 1319-1335, 2015
Các cơ quan ủy nhiệm: National Natural Science Foundation of China
Flight-dynamics and flutter modeling and analyses of a flexible flying-wing drone-invited
DK Schmidt, W Zhao, RK Kapania
AIAA Atmospheric Flight Mechanics Conference, 1748, 2016
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Comparative assessment of strut-braced and truss-braced wing configurations using multidisciplinary design optimization
I Chakraborty, T Nam, JR Gross, DN Mavris, JA Schetz, RK Kapania
Journal of Aircraft 52 (6), 2009-2020, 2015
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Modeling, design, and flight testing of three flutter controllers for a flying-wing drone
DK Schmidt, BP Danowsky, A Kotikalpudi, J Theis, CD Regan, PJ Seiler, ...
Journal of Aircraft 57 (4), 615-634, 2020
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Free vibration of curvilinearly stiffened shallow shells
P Shi, RK Kapania, CY Dong
Journal of Vibration and Acoustics 137 (3), 031006, 2015
Các cơ quan ủy nhiệm: National Natural Science Foundation of China
Global-local aeroelastic optimization of internal structure of transport aircraft wing
M Jrad, S De, RK Kapania
18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 4321, 2017
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Flight-dynamics and flutter analysis and control of an MDAO-designed flying-wing research drone
DK Schmidt, BP Danowsky, PJ Seiler, RK Kapania
AIAA scitech 2019 forum, 1816, 2019
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Stochastic fracture response and crack growth analysis of laminated composite edge crack beams using extended finite element method
A Lal, SB Mulani, RK Kapania
International journal of applied mechanics 9 (04), 1750061, 2017
Các cơ quan ủy nhiệm: Department of Science & Technology, India
A sensitivity-based nonlinear finite element model updating method for nonlinear engineering structures
Z Cao, Q Fei, D Jiang, RK Kapania, S Wu, H Jin
Applied Mathematical Modelling 100, 632-655, 2021
Các cơ quan ủy nhiệm: National Natural Science Foundation of China
Nonstationary random vibration analysis of wing with geometric nonlinearity under correlated excitation
Y Li, SB Mulani, RK Kapania, Q Fei, S Wu
Journal of Aircraft 55 (5), 2078-2091, 2018
Các cơ quan ủy nhiệm: National Natural Science Foundation of China
BLP optimization of composite flying-wings with sparibs and multiple control surfaces
W Zhao, RK Kapania
2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2018
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Static aeroelastic optimization of aircraft wing with multiple surfaces
W Zhao, RK Kapania
18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 4320, 2017
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Transonic aerodynamics analysis for multidisciplinary design optimization applications
M Segee, JA Schetz, RK Kapania
34th AIAA Applied Aerodynamics Conference, 4039, 2016
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Fuel Weight Minimization for Large N+ 3 Composite Transports with Multiple Control Surfaces
W Zhao, R Gupta, RK Kapania, DK Schmidt
AIAA SciTech 2020 Forum, 0663, 2020
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Stochastic critical stress intensity factor response of single edge notched laminated composite plate
A Lal, RK Kapania
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2013
Các cơ quan ủy nhiệm: Department of Science & Technology, India
Integrated aircraft parametric structural & outer mold line geometry modeling software
NJ Love, RK Kapania, DL Allison
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017
Các cơ quan ủy nhiệm: US Department of Defense
Investigation of controllability gramian as control objective in MDAO framework
R Gupta, W Zhao, RK Kapania
AIAA Aviation 2019 Forum, 3550, 2019
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Transonic aeroelastic analysis for multidisciplinary design optimization applications
W Mallik, RK Kapania, JA Schetz
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2016
Các cơ quan ủy nhiệm: US National Aeronautics and Space Administration
Finite element approach to the static, vibration and buckling analysis of curvilinearly stiffened plates
P Shi, RK Kapania, C Dong
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2015
Các cơ quan ủy nhiệm: National Natural Science Foundation of China
Lowest twelve frequencies of sandwich plates using third-order shear-normal deformation theory
B Alanbay, RC Batra, RK Kapania
AIAA Journal 58 (4), 1821-1835, 2020
Các cơ quan ủy nhiệm: US Department of Defense
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