Vibration Analysis of Curvilinearly Stiffened Composite Panel Subjected to In-Plane Loads
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[1] M. Mukhopadhyay,et al. A new finite element for buckling analysis of laminated stiffened plates , 1999 .
[2] Abdul Hamid Sheikh,et al. Buckling and dynamic instability analysis of stiffened shell panels , 2006 .
[3] K. C. Biswal,et al. Finite element analysis for stiffened laminated plates using higher order shear deformation theory , 1994 .
[4] S. Timoshenko. Theory of Elastic Stability , 1936 .
[5] Rakesh K. Kapania,et al. Vibration of Plate with Curvilinear Stiffeners Using Mesh-Free Method , 2009 .
[6] Rakesh K. Kapania,et al. Buckling and Static Analysis of Curvilinearly Stiffened Plates Using Mesh-Free Method , 2009 .
[7] Sameer B. Mulani,et al. Global/Local Optimization of Aircraft Wing Using Parallel Processing , 2016 .
[8] Paul M. Weaver,et al. Buckling analysis of stiffened variable angle tow panels , 2014 .
[9] Rakesh K. Kapania,et al. Buckling analysis of unitized curvilinearly stiffened composite panels , 2016 .
[10] Renato Vitaliani,et al. On the polynomial convergent formulation of a C0 isoparametric skew beam element , 1988 .
[11] B. Gangadhara Prusty,et al. Analysis of stiffened shell for ships and ocean structures by finite element method , 2001 .
[12] Eugenio Oñate,et al. Structural Analysis with the Finite Element Method Linear Statics , 2013 .
[13] Alex Velicki,et al. Future of Flight Vehicle Structures (2000 to 2023) , 2004 .
[14] Jing Li,et al. Optimal Design of Unitized Panels with Curvilinear Stiffeners , 2005 .
[15] Donald Paul,et al. Flight Vehicle Composite Structures , 2008 .
[16] M. Mukhopadhyay,et al. A new triangular stiffened plate element for laminate analysis , 2000 .
[17] J. Reddy. Mechanics of laminated composite plates : theory and analysis , 1997 .
[18] Rakesh K. Kapania,et al. Recent advances in analysis of laminated beams and plates. Part I - Sheareffects and buckling. , 1989 .
[19] R. Kapania,et al. Vibrational Analysis of Unitized Curvilinearly Stiffened Composite Panels Subjected to In-plane Loads , 2016 .
[20] B. Gangadhara Prusty,et al. FINITE ELEMENT TRANSIENT DYNAMIC ANALYSIS OF LAMINATED STIFFENED SHELLS , 2001 .
[21] Dawn C. Jegley,et al. Status of Advanced Stitched Unitized Composite Aircraft Structures , 2013 .
[22] Rolands Rikards,et al. Analysis for buckling and vibrations of composite stiffened shells and plates , 2001 .
[23] Rakesh K. Kapania,et al. EBF3PanelOpt: An optimization framework for curvilinear blade-stiffened panels , 2013 .
[24] Rakesh K. Kapania,et al. Wing-Box Weight Optimization Using Curvilinear Spars and Ribs (SpaRibs) , 2011 .
[25] In Lee,et al. Vibration analysis of anisotropic plates with eccentric stiffeners , 1995 .
[26] M. Mukhopadhyay,et al. Finite element free vibration of eccentrically stiffened plates , 1988 .
[27] J. N. Reddy,et al. Buckling and vibration of laminated composite plates using various plate theories , 1989 .
[28] K. C. Biswal,et al. Free-vibration analysis of stiffened laminated plates using higher-order shear deformation theory , 1996 .
[29] Rakesh K. Kapania,et al. Vibration and Buckling Analysis of Curvilinearly Stiffened Plates Using Finite Element Method , 2015 .
[30] Chunhui Yang,et al. Recent developments in finite element analysis for laminated composite plates , 2009 .
[31] Anand Srivastava,et al. First ply failure analysis of laminated stiffened plates , 2003 .
[32] M. Mukhopadhyay,et al. Transient response analysis of laminated stiffened plates , 2002 .