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Rakesh K. Kapania
Rakesh K. Kapania
Mitchell Professor, Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State
Bestätigte E-Mail-Adresse bei vt.edu
Titel
Zitiert von
Zitiert von
Jahr
Recent advances in analysis of laminated beams and plates. Part I-Sheareffects and buckling.
RK Kapania, S Raciti
AIAA journal 27 (7), 923-935, 1989
6111989
A survey of recent shell finite elements
HTY Yang, S Saigal, A Masud, RK Kapania
International Journal for numerical methods in engineering 47 (1‐3), 101-127, 2000
4182000
Recent advances in analysis of laminated beams and plates, Part II: Vibrations and wave propagation
RK Kapania, S Raciti
AIAA journal 27 (7), 935-946, 1989
3391989
Free vibration analysis of laminated plates using a layerwise theory
A Nosier, RK Kapania, JN Reddy
AIAA journal 31 (12), 2335-2346, 1993
2881993
A review on the analysis of laminated shells
RK Kapania
2051989
Optimal design of unitized panels with curvilinear stiffeners
R Kapania, J Li, H Kapoor
AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems …, 2005
1332005
Structural and aeroelastic modeling of general planform wings with morphing airfoils
FH Gern, DJ Inman, RK Kapania
AIAA journal 40 (4), 628-637, 2002
1322002
Wing-box weight optimization using curvilinear spars and ribs (SpaRibs)
D Locatelli, SB Mulani, RK Kapania
Journal of Aircraft 48 (5), 1671-1684, 2011
1282011
Design optimization of a truss-braced-wing transonic transport aircraft
O Gur, M Bhatia, JA Schetz, WH Mason, RK Kapania, DN Mavris
Journal of aircraft 47 (6), 1907-1917, 2010
1282010
EBF3PanelOpt: An optimization framework for curvilinear blade-stiffened panels
SB Mulani, WCH Slemp, RK Kapania
Thin-Walled Structures 63, 13-26, 2013
1222013
Buckling analysis of unitized curvilinearly stiffened composite panels
W Zhao, RK Kapania
Composite Structures 135, 365-382, 2016
1152016
Geometrically nonlinear NURBS isogeometric finite element analysis of laminated composite plates
H Kapoor, RK Kapania
Composite Structures 94 (12), 3434-3447, 2012
1132012
Thermal buckling of curvilinearly stiffened laminated composite plates with cutouts using isogeometric analysis
B Devarajan, RK Kapania
Composite Structures 238, 111881, 2020
1122020
Geometrically nonlinear finite element analysis of imperfect laminated shells
S Saigal, RK Kapania, TY Yang
Journal of Composite Materials 20 (2), 197-214, 1986
1111986
Nonlinear vibrations of unsymmetrically laminated beams
RK Kapania, S Raciti
AIAA journal 27 (2), 201-210, 1989
1011989
A shear-deformable beam element for the analysis of laminated composites
VK Goyal, RK Kapania
Finite Elements in Analysis and Design 43 (6-7), 463-477, 2007
922007
Conceptual design studies of a strut-braced wing transonic transport
JF Gundlach IV, PA Tetrault, FH Gern, AH Nagshineh-Pour, A Ko, ...
Journal of aircraft 37 (6), 976-983, 2000
922000
Development of a framework for truss-braced wing conceptual MDO
O Gur, M Bhatia, WH Mason, JA Schetz, RK Kapania, T Nam
Structural and Multidisciplinary optimization 44, 277-298, 2011
912011
Computation of actuation power requirements for smart wings with morphing airfoils
FH Gern, DJ Inman, RK Kapania
AIAA journal 43 (12), 2481-2486, 2005
872005
On a geometrically exact curved/twisted beam theory under rigid cross-section assumption
RK Kapania, J Li
Computational Mechanics 30 (5), 428-443, 2003
862003
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