| Year |
Citation |
Score |
| 2020 |
Alanbay B, Kapania RK, Batra RC. Free Vibration of Thick Quadrilateral Laminates Using Third-Order Shear-Normal Deformation Theory Aiaa Journal. 1-15. DOI: 10.2514/1.J059592 |
0.347 |
|
| 2020 |
Alanbay B, Batra RC, Kapania RK. Lowest Twelve Frequencies of Sandwich Plates Using Third-Order Shear-Normal Deformation Theory Aiaa Journal. 58: 1821-1835. DOI: 10.2514/1.J058920 |
0.327 |
|
| 2020 |
Lal A, Mulani SB, Kapania RK. Stochastic critical stress intensity factor response of single edge notched laminated composite plate using displacement correlation method Mechanics of Advanced Materials and Structures. 27: 1223-1237. DOI: 10.1080/15376494.2018.1506067 |
0.305 |
|
| 2020 |
Alanbay B, Kapania RK, Batra RC. Up to lowest 100 frequencies of rectangular plates using Jacobi polynomials and TSNDT Journal of Sound and Vibration. 480: 115352. DOI: 10.1016/J.Jsv.2020.115352 |
0.422 |
|
| 2020 |
Devarajan B, Kapania RK. Thermal buckling of curvilinearly stiffened laminated composite plates with cutouts using isogeometric analysis Composite Structures. 238: 111881. DOI: 10.1016/J.Compstruct.2020.111881 |
0.437 |
|
| 2019 |
De S, Jrad M, Kapania RK. Structural Optimization of Internal Structure of Aircraft Wings with Curvilinear Spars and Ribs Journal of Aircraft. 56: 707-718. DOI: 10.2514/1.C034818 |
0.323 |
|
| 2018 |
Mallik W, Schetz JA, Kapania RK. Rapid Transonic Flutter Analysis for Aircraft Conceptual Design Applications Aiaa Journal. 56: 2389-2402. DOI: 10.2514/1.J056218 |
0.345 |
|
| 2018 |
Li Y, Mulani SB, Kapania RK, Fei Q, Wu S. Nonstationary Random Vibration Analysis of Wing with Geometric Nonlinearity Under Correlated Excitation Journal of Aircraft. 55: 2078-2091. DOI: 10.2514/1.C034721 |
0.362 |
|
| 2017 |
Morris CC, Sultan C, Schetz JA, Kapania RK. State Variance-Based Approach to Flight Dynamic Constraints in Multidisciplinary Design Optimization Journal of Guidance Control and Dynamics. 40: 1206-1220. DOI: 10.2514/1.G002278 |
0.361 |
|
| 2017 |
Mallik W, Kapania RK, Schetz JA. Aeroelastic Applications of a Variable-Geometry Raked Wingtip Journal of Aircraft. 54: 62-74. DOI: 10.2514/1.C033805 |
0.355 |
|
| 2017 |
Soliman HE, Kapania RK. Equivalent constitutive behavior of sandwich cellular cores Journal of Sandwich Structures and Materials. 19: 1099636215613486. DOI: 10.1177/1099636215613486 |
0.349 |
|
| 2017 |
Lal A, Mulani SB, Kapania RK. Stochastic Fracture Response and Crack Growth Analysis of Laminated Composite Edge Crack Beams Using Extended Finite Element Method International Journal of Applied Mechanics. 9: 1750061. DOI: 10.1142/S1758825117500612 |
0.313 |
|
| 2017 |
Li Y, Mulani SB, Kapania RK, Fei Q, Wu S. Non-stationary random vibration analysis of structures under multiple correlated normal random excitations Journal of Sound and Vibration. 400: 481-507. DOI: 10.1016/J.Jsv.2017.04.006 |
0.341 |
|
| 2017 |
Li T, Kapania RK. On the formulation of a high-order discontinuous finite element method based on orthogonal polynomials for laminated plate structures International Journal of Mechanical Sciences. 149: 530-548. DOI: 10.1016/J.Ijmecsci.2017.08.006 |
0.403 |
|
| 2017 |
Lal A, Palekar SP, Mulani SB, Kapania RK. Stochastic extended finite element implementation for fracture analysis of laminated composite plate with a central crack Aerospace Science and Technology. 60: 131-151. DOI: 10.1016/J.Ast.2016.10.028 |
0.322 |
|
| 2016 |
Liu Q, Jrad M, Mulani SB, Kapania RK. Global/Local Optimization of Aircraft Wing Using Parallel Processing Aiaa Journal. 54: 3338-3348. DOI: 10.2514/1.J054499 |
0.34 |
|
| 2016 |
Reddy Sudalagunta P, Sultan C, Kapania RK, Watson LT, Raj P. Accurate Computing of Higher Vibration Modes of Thin Flexible Structures Aiaa Journal. 54: 1704-1718. DOI: 10.2514/1.J054428 |
0.349 |
|
| 2016 |
Ahmad N, Kapania RK. Free vibration analysis of integrally stiffened plates with plate-strip stiffeners Aiaa Journal. 54: 1103-1115. DOI: 10.2514/1.J054372 |
0.445 |
|
| 2016 |
Li Y, Mulani SB, Scott KML, Kapania RK, Wu S, Fei Q. Non-stationary random vibration analysis of multi degree systems using auto-covariance orthogonal decomposition Journal of Sound and Vibration. 372: 147-167. DOI: 10.1016/J.Jsv.2016.02.018 |
0.335 |
|
| 2015 |
Shi P, Kapania RK, Dong CY. Vibration and Buckling Analysis of Curvilinearly Stiffened Plates Using Finite Element Method Aiaa Journal. 53: 1319-1335. DOI: 10.2514/1.J053358 |
0.458 |
|
| 2015 |
Chakraborty I, Nam T, Gross JR, Mavris DN, Schetz JA, Kapania RK. Comparative assessment of strut-braced and truss-braced wing configurations using multidisciplinary design optimization Journal of Aircraft. 52: 2009-2020. DOI: 10.2514/1.C033120 |
0.37 |
|
| 2015 |
Mallik W, Kapania RK, Schetz JA. Effect of flutter on the multidisciplinary design optimization of truss-braced-wing aircraft Journal of Aircraft. 52: 1858-1872. DOI: 10.2514/1.C033096 |
0.31 |
|
| 2015 |
Joshi P, Mulani SB, Kapania RK. Experimental validation of the ebf3panelopt vibroacoustic analysis of stiffened panels Journal of Aircraft. 52: 1481-1491. DOI: 10.2514/1.C032982 |
0.441 |
|
| 2015 |
Jrad M, Mulani S, Kapania R. A Framework for Damage Tolerance and Optimization of Stiffened Panels Structural Health Monitoring-An International Journal. DOI: 10.12783/Shm2015/3 |
0.393 |
|
| 2015 |
Shi P, Kapania RK, Dong CY. Free Vibration of Curvilinearly Stiffened Shallow Shells Journal of Vibration and Acoustics. 137: 31006. DOI: 10.1115/1.4029360 |
0.426 |
|
| 2015 |
Joshi P, Mulani SB, Kapania RK. Multi-objective vibro-acoustic optimization of stiffened panels Structural and Multidisciplinary Optimization. 51: 835-848. DOI: 10.1007/S00158-014-1177-9 |
0.358 |
|
| 2014 |
Slemp WCH, Kapania RK. Beam Delamination by Integrated Local Petrov–Galerkin Sinc Method Aiaa Journal. 52: 419-435. DOI: 10.2514/1.J052573 |
0.384 |
|
| 2014 |
Shirley CM, Schetz JA, Kapania RK, Haftka RT. Tradeoffs of wing weight and lift/drag in design of medium-range transport aircraft Journal of Aircraft. 51: 904-912. DOI: 10.2514/1.C032605 |
0.315 |
|
| 2014 |
Islam MM, Kapania RK. Global–Local Finite Element Analysis of Adhesive Joints and Crack Propagation Journal of Aircraft. 51: 310-319. DOI: 10.2514/1.C032387 |
0.373 |
|
| 2014 |
Morris CC, Allison DL, Schetz JA, Kapania RK, Sultan C. Parametric geometry model for design studies of tailless supersonic aircraft Journal of Aircraft. 51: 1455-1466. DOI: 10.2514/1.C032340 |
0.328 |
|
| 2014 |
Locatelli D, Mulani SB, Kapania RK. Parameterization of Curvilinear Spars and Ribs for Optimum Wing Structural Design Journal of Aircraft. 51: 532-546. DOI: 10.2514/1.C032249 |
0.4 |
|
| 2014 |
Kunaporn C, Singh MP, Patil MJ, Kapania RK. Aeroelastic divergence of a randomly cracked thin-walled beam Journal of Aircraft. 51: 390-401. DOI: 10.2514/1.C031885 |
0.316 |
|
| 2014 |
McQuigg TD, Kapania RK, Scotti SJ, Walker SP. Compression after impact analysis on thin face sheet honeycomb core sandwich panels Journal of Spacecraft and Rockets. 51: 200-212. DOI: 10.2514/1.A32428 |
0.348 |
|
| 2014 |
Tamijani AY, Mulani SB, Kapania RK. A framework combining meshfree analysis and adaptive kriging for optimization of stiffened panels Structural and Multidisciplinary Optimization. 49: 577-594. DOI: 10.1007/S00158-013-0993-7 |
0.402 |
|
| 2013 |
Mulani SB, Havens D, Norris A, Bird RK, Kapania RK, Olliffe R. Design, optimization, and evaluation of Al-2139 compression panel with integral T-stiffeners Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/1.C032199 |
0.422 |
|
| 2013 |
Ghoman SS, Wang Z, Chen PC, Kapania RK. Hybrid Optimization Framework with Proper-Orthogonal-Decomposition-Based Order Reduction and Design-Space Evolution Scheme Journal of Aircraft. 50: 1776-1786. DOI: 10.2514/1.C032151 |
0.352 |
|
| 2013 |
Islam MM, Kapania RK. Fracture Analysis of a Curvilinearly Stiffener Panel Subjected to Multiple Combined Loadings Journal of Aircraft. 50: 1576-1592. DOI: 10.2514/1.C032071 |
0.382 |
|
| 2013 |
Mulani SB, Duggirala V, Kapania RK. Curvilinearly T-Stiffened Panel-Optimization Framework Under Multiple Load Cases Using Parallel Processing Journal of Aircraft. 50: 1540-1554. DOI: 10.2514/1.C032064 |
0.426 |
|
| 2013 |
Mulani SB, Slemp WCH, Kapania RK. EBF3PanelOpt: An optimization framework for curvilinear blade-stiffened panels Thin-Walled Structures. 63: 13-26. DOI: 10.1016/J.Tws.2012.09.008 |
0.452 |
|
| 2013 |
Kapoor H, Kapania RK, Soni SR. Interlaminar stress calculation in composite and sandwich plates in NURBS Isogeometric finite element analysis Composite Structures. 106: 537-548. DOI: 10.1016/J.Compstruct.2013.05.028 |
0.368 |
|
| 2012 |
Kunaporn C, Singh MP, Patil MJ, Kapania RK. Analysis of thin-walled beam with crack of random location and size Aiaa Journal. 50: 1265-1280. DOI: 10.2514/1.J051244 |
0.359 |
|
| 2012 |
Tamijani AY, Kapania RK. Chebyshev-Ritz Approach to Buckling and Vibration of Curvilinearly Stiffened Plate Aiaa Journal. 50: 1007-1018. DOI: 10.2514/1.J050042 |
0.397 |
|
| 2012 |
Meadows NA, Schetz JA, Kapania RK, Bhatia M, Seber G. Multidisciplinary design optimization of medium-range transonic truss-braced wing transport aircraft Journal of Aircraft. 49: 1844-1856. DOI: 10.2514/1.C031695 |
0.315 |
|
| 2012 |
Bhatia M, Kapania RK, Haftka RT. Structural and Aeroelastic Characteristics of Truss-Braced Wings: A Parametric Study Journal of Aircraft. 49: 302-310. DOI: 10.2514/1.C031556 |
0.377 |
|
| 2012 |
Ghoman SS, Kapania RK, Chen PC, Sarhaddi D, Lee DH. Multifidelity, Multistrategy, and Multidisciplinary Design Optimization Environment Journal of Aircraft. 49: 1255-1270. DOI: 10.2514/1.C031507 |
0.314 |
|
| 2012 |
Joshi P, Mulani SB, Slemp WCH, Kapania RK. Vibro-Acoustic Optimization of Turbulent Boundary Layer Excited Panel with Curvilinear Stiffeners Journal of Aircraft. 49: 52-65. DOI: 10.2514/1.C031105 |
0.374 |
|
| 2012 |
Tamijani AY, Kapania RK. Vibration Analysis of Curvilinearly-Stiffened Functionally Graded Plate Using Element Free Galerkin Method Mechanics of Advanced Materials and Structures. 19: 100-108. DOI: 10.1080/15376494.2011.572240 |
0.418 |
|
| 2012 |
Kapoor H, Kapania RK. Geometrically nonlinear NURBS isogeometric finite element analysis of laminated composite plates Composite Structures. 94: 3434-3447. DOI: 10.1016/J.Compstruct.2012.04.028 |
0.42 |
|
| 2011 |
Kunaporn C, Singh MP, Patil MJ, Kapania RK. Random propagation of a crack in a thin-walled beam Journal of Aircraft. 48: 2002-2011. DOI: 10.2514/1.C031424 |
0.312 |
|
| 2011 |
Locatelli D, Mulani SB, Kapania RK. Wing-Box Weight Optimization Using Curvilinear Spars and Ribs (SpaRibs) Journal of Aircraft. 48: 1671-1684. DOI: 10.2514/1.C031336 |
0.378 |
|
| 2011 |
Tamijani AY, Kapania RK. Random Response Analysis of Curvilinearly Stiffened Plates Using Element-Free Galerkin Method Journal of Aircraft. 48: 1856-1863. DOI: 10.2514/1.C031132 |
0.405 |
|
| 2011 |
Slemp WCH, Bird RK, Kapania RK, Havens D, Norris A, Olliffe R. Design, Optimization, and Evaluation of Integrally Stiffened Al-7050 Panel with Curved Stiffeners Journal of Aircraft. 48: 1163-1175. DOI: 10.2514/1.C031118 |
0.454 |
|
| 2011 |
Bhatia M, Kapania RK, Evans D. Comparative Study on Optimal Stiffener Placement for Curvilinearly Stiffened Panels Journal of Aircraft. 48: 77-91. DOI: 10.2514/1.C000234 |
0.4 |
|
| 2011 |
Dillard DA, Pohlit DJ, Jacob GC, Starbuck JM, Kapania RK. On the Use of a Driven Wedge Test to Acquire Dynamic Fracture Energies of Bonded Beam Specimens Journal of Adhesion. 87: 395-423. DOI: 10.1080/00218464.2011.562125 |
0.314 |
|
| 2011 |
Dang TD, Kapania RK, Patil MJ. Ritz analysis of discontinuous beams using local trigonometric functions Computational Mechanics. 47: 235-250. DOI: 10.1007/S00466-010-0540-Y |
0.354 |
|
| 2011 |
Gur O, Bhatia M, Mason WH, Schetz JA, Kapania RK, Nam T. Development of a framework for truss-braced wing conceptual MDO Structural and Multidisciplinary Optimization. 44: 277-298. DOI: 10.1007/S00158-010-0612-9 |
0.358 |
|
| 2010 |
Slemp WCH, Mulani SB, Kapania RK. Elastic-Plastic Analysis by Integrated Local Petrov-Galerkin Sinc Method Aiaa Journal. 48: 2084-2098. DOI: 10.2514/1.J050281 |
0.387 |
|
| 2010 |
Mulani SB, Kapania RK, Scott KML. Generalized Linear Random Vibration Analysis Using Autocovariance Orthogonal Decomposition Aiaa Journal. 48: 1652-1661. DOI: 10.2514/1.J050033 |
0.343 |
|
| 2010 |
Dang TD, Kapania RK, Slemp WCH, Bhatia M, Gurav SP. Optimization and Postbuckling Analysis of Curvilinear-Stiffened Panels Under Multiple-Load Cases Journal of Aircraft. 47: 1656-1671. DOI: 10.2514/1.C000249 |
0.428 |
|
| 2010 |
Gur O, Bhatia M, Schetz JA, Mason WH, Kapania RK, Mavris DN. Design optimization of a truss-braced-wing transonic transport aircraft Journal of Aircraft. 47: 1907-1917. DOI: 10.2514/1.47546 |
0.339 |
|
| 2010 |
Mulani SB, Joshi P, Li J, Kapania RK, Shin YS. Optimal Design of Unitized Structures Using Response Surface Approaches Journal of Aircraft. 47: 1898-1906. DOI: 10.2514/1.47411 |
0.419 |
|
| 2010 |
Dang TD, Kapania RK, Patil MJ. Analytical modeling of cracked thin-walled beams under torsion Aiaa Journal. 48: 664-675. DOI: 10.2514/1.45393 |
0.38 |
|
| 2010 |
Joshi P, Mulani SB, Gurav SP, Kapania RK. Design Optimization for Minimum Sound Radiation from Point-Excited Curvilinearly Stiffened Panel Journal of Aircraft. 47: 1100-1110. DOI: 10.2514/1.44778 |
0.413 |
|
| 2010 |
Tamijani AY, McQuigg T, Kapania RK. Free Vibration Analysis of Curvilinear-Stiffened Plates and Experimental Validation Journal of Aircraft. 47: 192-200. DOI: 10.2514/1.44613 |
0.415 |
|
| 2009 |
Scott KML, McQuigg TD, Mulani SB, Kapania RK, Schetz JA. Flow induced vibrations of pressure/temperature sensors Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/1.45016 |
0.313 |
|
| 2009 |
Tamijani AY, Kapania RK. Buckling and Static Analysis of Curvilinearly Stiffened Plates Using Mesh-Free Method Aiaa Journal. 48: 2739-2751. DOI: 10.2514/1.43917 |
0.416 |
|
| 2009 |
Tamijani AY, Kapania RK. Vibration of Plate with Curvilinear Stiffeners Using Mesh-Free Method Aiaa Journal. 48: 1569-1581. DOI: 10.2514/1.43082 |
0.446 |
|
| 2009 |
Slemp WCH, Kapania RK. Imposing boundary conditions in Sinc method using highest derivative approximation Journal of Computational and Applied Mathematics. 230: 371-392. DOI: 10.1016/J.Cam.2008.12.006 |
0.38 |
|
| 2008 |
Slemp WCH, Kapania RK. Interlaminar Stresses by Sinc Method Based on Interpolation of the Highest Derivative Aiaa Journal. 46: 3128-3141. DOI: 10.2514/1.39613 |
0.428 |
|
| 2008 |
Kapania RK, Soliman HE, Vasudeva S, Hughes O, Makhecha DP. Static Analysis of Sandwich Panels with Square Honeycomb Core Aiaa Journal. 46: 627-634. DOI: 10.2514/1.28121 |
0.751 |
|
| 2008 |
Slemp WCH, Hallauer WLJ, Kapania RK. Estimation of viscous and Coulomb damping from free-vibration data by a least-squares curve-fitting analysis Smart Structures and Systems. 4: 279-290. DOI: 10.12989/Sss.2008.4.3.279 |
0.335 |
|
| 2008 |
Goyal VK, Kapania RK. Dynamic stability of laminated beams subjected to nonconservative loading Thin-Walled Structures. 46: 1359-1369. DOI: 10.1016/J.Tws.2008.03.014 |
0.693 |
|
| 2008 |
Goyal VK, Kapania RK. Dynamic stability of uncertain laminated beams subjected to subtangential loads International Journal of Solids and Structures. 45: 2799-2817. DOI: 10.1016/J.Ijsolstr.2007.11.024 |
0.706 |
|
| 2007 |
Goyal VK, Kapania RK. A shear-deformable beam element for the analysis of laminated composites Finite Elements in Analysis and Design. 43: 463-477. DOI: 10.1016/J.Finel.2006.11.011 |
0.717 |
|
| 2006 |
Sheng L, Kapania RK. Extensive experiments on genetic algorithms for the optimization of piezoelectric actuator locations Aiaa Journal. 44: 2904-2918. DOI: 10.2514/1.19181 |
0.581 |
|
| 2006 |
Kapoor H, Chun S, Motley MR, Kapania RK, Plaut RH. Nonlinear Response of Highly Flexible Structures to Air Blast Loads: Application Shelters Aiaa Journal. 44: 2034-2042. DOI: 10.2514/1.18480 |
0.413 |
|
| 2006 |
Kapania RK, Kim Y. Flexural-torsional coupled vibration of slewing beams using various types of orthogonal polynomials Journal of Mechanical Science and Technology. 20: 1790-1800. DOI: 10.1007/Bf03027573 |
0.404 |
|
| 2006 |
Kim YY, Kapania RK, Johnson ER, Palmer ME, Kwon TK, Hong CU, Kim NG. Dynamic analysis and structural optimization of a fiber optic sensor using neural networks Journal of Mechanical Science and Technology. 20: 251-261. DOI: 10.1007/Bf02915827 |
0.315 |
|
| 2005 |
Ba-Abbad MA, Kapania RK, Nikolaidis E. A new approach for system reliability-based design optimization Sae Technical Papers. DOI: 10.4271/2005-01-0348 |
0.385 |
|
| 2005 |
Soliman HE, Kapania RK. Probability of Failure of Composite Cylinders Subjected to Axisymmetric Loading Aiaa Journal. 43: 1342-1348. DOI: 10.2514/1.10074 |
0.331 |
|
| 2004 |
Kapania RK, Chun S. Preliminary Design of a Structural Wing Box Under a Twist Constraint Part I Journal of Aircraft. 41: 1230-1239. DOI: 10.2514/1.699 |
0.454 |
|
| 2004 |
Natarajan A, Kapania RK, Inman DJ. Aeroelastic Optimization of Adaptive Bumps for Yaw Control Journal of Aircraft. 41: 175-185. DOI: 10.2514/1.477 |
0.745 |
|
| 2004 |
Li J, Kapania RK. Load Updating for Nonlinear Finite Element Models Aiaa Journal. 45: 1444-1458. DOI: 10.2514/1.19073 |
0.457 |
|
| 2004 |
Kapania RK. Review of Vibration of Laminated Shells and Plates Aiaa Journal. 42: 1946-1947. DOI: 10.2514/1.14207 |
0.303 |
|
| 2004 |
Natarajan A, Kapania RK, Inman DJ. Analysis of Time-Varient Aeroelastic Systems Using Neural Network Aiaa Journal. 42: 1933-1936. DOI: 10.2514/1.10601 |
0.665 |
|
| 2003 |
Ba-abbad MA, Kapania RK, Nikolaidis E. Reliability-based structural optimization of an elastic-plastic beam Aiaa Journal. 41: 1573-1582. DOI: 10.2514/2.2110 |
0.689 |
|
| 2003 |
Kim YY, Kapania RK. Neural Networks for Inverse Problems Using Principal Component Analysis and Orthogonal Arrays Aiaa Journal. 44: 1628-1634. DOI: 10.2514/1.10641 |
0.356 |
|
| 2003 |
Kapania RK, Li J. A Formulation And Implementation Of Geometrically Exact Curved Beam Elements Incorporating Finite Strains And Finite Rotations Computational Mechanics. 30: 444-459. DOI: 10.1007/S00466-003-0422-7 |
0.453 |
|
| 2003 |
Kapania RK, Li J. On a geometrically exact curved/twisted beam theory under rigid cross-section assumption Computational Mechanics. 30: 428-443. DOI: 10.1007/S00466-003-0421-8 |
0.37 |
|
| 2002 |
Chock JMK, Kapania RK. Load Updating for Finite Element Models Aiaa Journal. 41: 1667-1673. DOI: 10.2514/2.7312 |
0.448 |
|
| 2002 |
Kapania RK, Sheng L. Toward More Effective Genetic Algorithms for the Optimization of Piezoelectric Actuator Locations Aiaa Journal. 40: 1246-1250. DOI: 10.2514/2.1782 |
0.598 |
|
| 2002 |
Gern FH, Inman DJ, Kapania RK. Structural and Aeroelastic Modeling of General Planform Wings with Morphing Airfoils Aiaa Journal. 40: 628-637. DOI: 10.2514/2.1719 |
0.368 |
|
| 2002 |
Magill S, MacLean M, Schetz J, Kapania R, Sang A, Pulliam W. Study of Direct-Measuring Skin-Friction Gauge with Rubber Sheet for Damping Aiaa Journal. 40: 50-57. DOI: 10.2514/2.1640 |
0.328 |
|
| 2002 |
Natarajan A, Kapania RK, Inman DJ. Near-Exact Analytical Solutions of Linear Time-Variant Systems Aiaa Journal. 40: 2362-2366. DOI: 10.2514/2.1577 |
0.676 |
|
| 2002 |
Kapania RK, Goyal VK. Free vibration of unsymmetrically laminated beams having uncertain ply orientations Aiaa Journal. 40: 2336-2344. DOI: 10.2514/2.1573 |
0.698 |
|
| 2001 |
Gern FH, Ko A, Sulaeman E, Gundlach JF, Kapania RK, Haftka RT. Multidisciplinary Design Optimization of a Transonic Commercial Transport with Strut-Braced Wing Journal of Aircraft. 38: 1006-1014. DOI: 10.2514/2.2887 |
0.401 |
|
| 2001 |
Gern FH, Naghshineh-Pour AH, Sulaeman E, Kapania RK, Haftka RT. Structural Wing Sizing for Multidisciplinary Design Optimization of a Strut-Braced Wing Journal of Aircraft. 38: 154-163. DOI: 10.2514/2.2747 |
0.39 |
|
| 2001 |
Sheng L, Kapania RK. Genetic algorithms for optimization of piezoelectric actuator locations Aiaa Journal. 39: 1818-1822. DOI: 10.2514/2.1519 |
0.596 |
|
| 2001 |
Liu Y, Kapania RK. Equivalent Skin Analysis of Wing Structures Using Neural Networks Aiaa Journal. 39: 1390-1399. DOI: 10.2514/2.1459 |
0.573 |
|
| 2001 |
Chock JMK, Kapania RK. Review of two methods for calculating explosive Air blast The Shock and Vibration Digest. 33: 91-102. DOI: 10.1177/058310240103300201 |
0.359 |
|
| 2000 |
Hammerand DC, Kapania RK. Geometrically Nonlinear Shell Element for Hygrothermorheologically Simple Linear Viscoelastic Composites Aiaa Journal. 38: 2305-2319. DOI: 10.2514/2.900 |
0.428 |
|
| 2000 |
Gundlach JF, Tetrault P, Gern FH, Nagshineh-Pour AH, Ko A, Schetz JA, Mason WH, Kapania RK, Grossman B, Haftka RT. Conceptual Design Studies of a Strut-Braced Wing Transonic Transport Journal of Aircraft. 37: 976-983. DOI: 10.2514/2.2724 |
0.369 |
|
| 2000 |
Liu Y, Kapania RK. Modal Response of Trapezoidal Wing Structures Using Second-Order Shape Sensitivities Aiaa Journal. 38: 732-735. DOI: 10.2514/2.1024 |
0.579 |
|
| 2000 |
Yang HTY, Saigal S, Masud A, Kapania RK. A survey of recent shell finite elements International Journal For Numerical Methods in Engineering. 47: 101-127. DOI: 10.1002/(Sici)1097-0207(20000110/30)47:1/3<101::Aid-Nme763>3.0.Co;2-C |
0.383 |
|
| 1999 |
Gern FH, Gundlach JF, Ko A, Naghshineh-Pour A, Sulaeman E, Tetrault PA, Grossman B, Kapania RK, Mason WH, Schetz JA, Haftka RT. Multidisciplinary design optimization of a transonic commercial transport with a strut-braced wing Sae Technical Papers. DOI: 10.4271/1999-01-5621 |
0.398 |
|
| 1999 |
Park S, Kapania RK, Kim SJ. Nonlinear Transient Response and Second-Order Sensitivity Using Time Finite Element Method Aiaa Journal. 37: 613-622. DOI: 10.2514/2.761 |
0.434 |
|
| 1999 |
Hammerand DC, Kapania RK. Thermoviscoelastic Analysis of Composite Structures Using a Triangular Flat Shell Element Aiaa Journal. 37: 238-247. DOI: 10.2514/2.696 |
0.431 |
|
| 1998 |
Mohan P, Kapania RK. Updated Lagrangian Formulation of a Flat Triangular Element for Thin Laminated Shells Aiaa Journal. 36: 273-281. DOI: 10.2514/2.7512 |
0.468 |
|
| 1998 |
Park S, Kapania RK. Comparison of Various Orthogonal Polynomials in hp-Version Time Finite Element Method Aiaa Journal. 36: 651-655. DOI: 10.2514/2.419 |
0.343 |
|
| 1998 |
Bhardwaj MK, Kapania RK, Reichenbach E, Guruswamy GP. Computational Fluid Dynamics/Computational Structural Dynamics Interaction Methodology for Aircraft Wings Aiaa Journal. 36: 2179-2186. DOI: 10.2514/2.342 |
0.327 |
|
| 1998 |
Kapania RK, Mohan P, Jakubowski A. Control of Thermal Deformations of Spherical Mirror Segment Journal of Spacecraft and Rockets. 35: 156-162. DOI: 10.2514/2.3323 |
0.328 |
|
| 1998 |
Kapania RK, Lovejoy AE. Free Vibration of Thick Generally Laminated Quadrilateral Plates Having Arbitrarily Located Point Supports Journal of Aircraft. 35: 958-965. DOI: 10.2514/2.2392 |
0.399 |
|
| 1998 |
Haryadi SG, Kapania RK, Haftka RT. Global/local analysis of composite plates with cracks Composites Part B-Engineering. 29: 271-276. DOI: 10.1016/S1359-8368(97)00034-6 |
0.318 |
|
| 1997 |
Issac JC, Kapania RK. Aeroelastic Sensitivity Analysis of Wings Using Automatic Differentiation Aiaa Journal. 35: 519-525. DOI: 10.2514/3.13534 |
0.456 |
|
| 1997 |
Kapania RK, Park S. Parametric identification of nonlinear structural dynamic systems using time finite element method Aiaa Journal. 35: 719-726. DOI: 10.2514/2.163 |
0.383 |
|
| 1997 |
Issac JC, Kapania RK. Aeroelastic Sensitivity Analysis of Wings Aiaa Journal. 35: 519-525. DOI: 10.2514/2.125 |
0.424 |
|
| 1997 |
Kapania RK, Haryadi SG, Haftka RT. Global/local analysis of composite plates with cutouts Computational Mechanics. 19: 386-396. DOI: 10.1007/S004660050187 |
0.398 |
|
| 1996 |
Kapania RK, Lovejoy AE. Free vibration of thick generally laminated cantilever quadrilateral plates Aiaa Journal. 34: 1474-1486. DOI: 10.2514/3.13256 |
0.417 |
|
| 1996 |
Kapania RK, Mohan P. Static, free vibration and thermal analysis of composite plates and shells using a flat triangular shell element Computational Mechanics. 17: 343-357. DOI: 10.1007/Bf00368557 |
0.425 |
|
| 1996 |
Kapania RK, Park S. Nonlinear transient response and its sensitivity using finite elements in time Computational Mechanics. 17: 306-317. DOI: 10.1007/Bf00368553 |
0.4 |
|
| 1995 |
Issac JC, Kapania RK, Barthelemy JM. Sensitivity of flutter response of a wing to shape and modal parameters Aiaa Journal. 33: 1983-1986. DOI: 10.2514/3.12758 |
0.301 |
|
| 1994 |
Kapania RK, Issac JC. Sensitivity Analysis of Aeroelastic Response of a Wing in Transonic Flow Aiaa Journal. 32: 350-356. DOI: 10.2514/3.59995 |
0.383 |
|
| 1994 |
Sankaranarayanan S, Haftka RT, Kapania RK. Truss Topology Optimization with Simultaneous Analysis and Design Aiaa Journal. 32: 420-424. DOI: 10.2514/3.12000 |
0.396 |
|
| 1994 |
Singhvi S, Kapania RK. Comparison Of Simple And Chebychev Polynomials In Rayleigh-Ritz Analysis Journal of Engineering Mechanics-Asce. 120: 2126-2135. DOI: 10.1061/(Asce)0733-9399(1994)120:10(2126) |
0.421 |
|
| 1994 |
Kapania RK, Stoumbos TG. Geometrically nonlinear impact response of thin laminated imperfect cylindrical panels Composites Engineering. 4: 397-416. DOI: 10.1016/S0961-9526(09)80014-2 |
0.373 |
|
| 1994 |
Nosier A, Kapania RK, Reddy JN. Forced vibration and low-velocity impact of laminated composite plates Sadhana. 19: 509-541. DOI: 10.1007/Bf02812166 |
0.398 |
|
| 1994 |
Nosier A, Kapania RK, Reddy JN. Low-velocity impact of laminated composites using a layerwise theory Computational Mechanics. 13: 360-379. DOI: 10.1007/Bf00512589 |
0.402 |
|
| 1993 |
Eldred LB, Kapania RK, Barthelemy JM. Sensitivity analysis of aeroelastic response of a wing using piecewise pressure representation Journal of Aircraft. 33: 803-807. DOI: 10.2514/3.47017 |
0.352 |
|
| 1993 |
Singhvi S, Kapania RK. Shape sensitivities and approximations of modal response of laminated skew plates Journal of Aircraft. 30: 423-426. DOI: 10.2514/3.46358 |
0.324 |
|
| 1993 |
Nosier A, Kapania RK, Reddy JN. Free vibration analysis of laminated plates using a layerwise theory Aiaa Journal. 31: 2335-2346. DOI: 10.2514/3.11933 |
0.343 |
|
| 1993 |
Kapania RK, Obst AW. A New Element for Symmetrically Laminated Cross-Ply Beams based on a Higher-Order Theory Manufacturing Research and Technology. 16: 147-156. DOI: 10.1016/B978-0-444-89856-2.50018-1 |
0.401 |
|
| 1993 |
Kapania RK, Byun C. Reduction methods based on eigenvectors and Ritz vectors for nonlinear transient analysis Computational Mechanics. 11: 65-82. DOI: 10.1007/Bf00370072 |
0.388 |
|
| 1992 |
Byun C, Kapania RK. Prediction of interlaminar stresses in laminated plates using globalorthogonal interpolation polynomials Aiaa Journal. 30: 2740-2749. DOI: 10.2514/3.11293 |
0.375 |
|
| 1992 |
Byun C, Kapania RK. Nonlinear impact response of thin imperfect laminated plates using a reduction method Composites Engineering. 2: 391-410. DOI: 10.1016/0961-9526(92)90034-4 |
0.408 |
|
| 1992 |
Obst AW, Kapania RK. Nonlinear static and transient finite element analysis of laminated beams Composites Engineering. 2: 375-389. DOI: 10.1016/0961-9526(92)90033-3 |
0.445 |
|
| 1992 |
Kapania RK, Singhvi S. Free vibration analyses of generally laminated tapered skew plates Composites Engineering. 2: 197-212. DOI: 10.1016/0961-9526(92)90004-P |
0.408 |
|
| 1992 |
Kapania RK, Byun C. Vibrations of imperfect laminated panels under complex preloads International Journal of Non-Linear Mechanics. 27: 51-62. DOI: 10.1016/0020-7462(92)90022-Y |
0.437 |
|
| 1991 |
Kapania RK, Bergen FD, Barthelemy JM. Shape sensitivity analysis of flutter response of a laminated wing Aiaa Journal. 29: 611-612. DOI: 10.2514/3.59930 |
0.33 |
|
| 1990 |
Kapania RK, Castel F. A Simple Element for Aeroelastic Analysis of Undamaged and Damaged Wings Aiaa Journal. 28: 329-337. DOI: 10.2514/3.10393 |
0.433 |
|
| 1990 |
Eldred LB, Kapania RK, Bosch HR. Preliminary investigations on the use of spectral methods for flow calculations Journal of Wind Engineering and Industrial Aerodynamics. 36: 1021-1027. DOI: 10.1016/0167-6105(90)90098-W |
0.316 |
|
| 1990 |
Kapania RK. Stability of cylindrical shells under combined wind and snow loads Journal of Wind Engineering and Industrial Aerodynamics. 36: 937-948. DOI: 10.1016/0167-6105(90)90090-Y |
0.379 |
|
| 1989 |
Kapania RK, Raciti S. Recent Advances in Analysis of Laminated Beams and Plates, Part II: Vibrations and Wave Propagation Aiaa Journal. 27: 935-946. DOI: 10.2514/3.59909 |
0.412 |
|
| 1989 |
Haftka RT, Kapania RK. Sensitivity of actively damped structures to imperfections and modeling errors Aiaa Journal. 27: 1434-1440. DOI: 10.2514/3.10282 |
0.338 |
|
| 1989 |
Kapania RK, Raciti S. Recent advances in analysis of laminated beams and plates. Part I - Sheareffects and buckling. Aiaa Journal. 27: 923-935. DOI: 10.2514/3.10202 |
0.455 |
|
| 1989 |
Yang TY, Kapania RK, Saigal S. Accurate rigid-body modes representation for a nonlinear curved thin-shell element Aiaa Journal. 27: 211-218. DOI: 10.2514/3.10083 |
0.407 |
|
| 1989 |
Kapania RK, Raciti S. Nonlinear vibrations of unsymmetrically laminated beams Aiaa Journal. 27: 201-210. DOI: 10.2514/3.10082 |
0.433 |
|
| 1989 |
Kapania RK, Wolfe DR. Buckling of Axially Loaded Beam-Plate With Multiple Delaminations Journal of Pressure Vessel Technology-Transactions of the Asme. 111: 151-158. DOI: 10.1115/1.3265651 |
0.37 |
|
| 1988 |
Kapania RK, Yang TY. Stability of wind-loaded cylindrical shells Journal of Wind Engineering and Industrial Aerodynamics. 28: 281-290. DOI: 10.1016/0167-6105(88)90124-9 |
0.41 |
|
| 1987 |
Kapania RK, Yang TY. Buckling, postbuckling, and nonlinear vibrations of imperfect plates Aiaa Journal. 25: 1338-1346. DOI: 10.2514/3.9788 |
0.43 |
|
| 1987 |
Saigal S, Yang TY, Kapania RK. Dynamic buckling of imperfection-sensitive shell structures Journal of Aircraft. 24: 718-724. DOI: 10.2514/3.45512 |
0.407 |
|
| 1986 |
Kapania RK, Yang TY. Formulation of an imperfect quadrilateral doubly curved shell element for postbuckling analysis Aiaa Journal. 24: 310-311. DOI: 10.2514/3.9261 |
0.416 |
|
| 1986 |
Saigal S, Kapania RK, Yang TY. Geometrically Nonlinear Finite Element Analysis of Imperfect Laminated Shells Journal of Composite Materials. 20: 197-214. DOI: 10.1177/002199838602000206 |
0.431 |
|
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