Add to ORKGTwo-dimensional static aerodynamics for determining supersonic flutter characteristics of simply supported isotropic sandwich panel
Experimental studies of panel flutter using thin metal plates were conducted at a Mach number of 1.3...
"Representative experimental results are presented to show the current status of the panel flutter p...
Design factors for flutter control of stiffened exterior skin panels for hypersonic aircraf
Numerical analysis of supersonic flutter of flat rectangular, biaxilly stressed sandwich panel
Flutter analysis on buckled supported rectangular panels under supersonic surface flo
Representative experimental results are presented to show the current status of the panel flutter pr...
The supersonic flutter of wide panels on discrete flexible supports is investigated for three differ...
Supersonic flutter analysis for flat loaded orthotropic panels with edge restrain
Flutter of flat rectangular panels based on three-dimensional supersonic potential flo
A modal flutter analysis for biaxially loaded, orthotropic panels, using linear piston-theory aerody...
The present study examines the problem of flutter of flat rectangular panels subjected to static inp...
Flutter analysis of flat rectangular panels based on three-dimensional supersonic unsteady potential...
Side edge boundary condition and transverse shear stiffness effects on orthotropic panel flutter in ...
The flutter of two-bay clamped-edge and simply supported panels at supersonic Mach numbers is studie...
Experiment and theory of supersonic flutter in panels - length/width and stress ratios to prevent fl...
Experimental studies of panel flutter using thin metal plates were conducted at a Mach number of 1.3...
"Representative experimental results are presented to show the current status of the panel flutter p...
Design factors for flutter control of stiffened exterior skin panels for hypersonic aircraf
Numerical analysis of supersonic flutter of flat rectangular, biaxilly stressed sandwich panel
Flutter analysis on buckled supported rectangular panels under supersonic surface flo
Representative experimental results are presented to show the current status of the panel flutter pr...
The supersonic flutter of wide panels on discrete flexible supports is investigated for three differ...
Supersonic flutter analysis for flat loaded orthotropic panels with edge restrain
Flutter of flat rectangular panels based on three-dimensional supersonic potential flo
A modal flutter analysis for biaxially loaded, orthotropic panels, using linear piston-theory aerody...
The present study examines the problem of flutter of flat rectangular panels subjected to static inp...
Flutter analysis of flat rectangular panels based on three-dimensional supersonic unsteady potential...
Side edge boundary condition and transverse shear stiffness effects on orthotropic panel flutter in ...
The flutter of two-bay clamped-edge and simply supported panels at supersonic Mach numbers is studie...
Experiment and theory of supersonic flutter in panels - length/width and stress ratios to prevent fl...
Experimental studies of panel flutter using thin metal plates were conducted at a Mach number of 1.3...
"Representative experimental results are presented to show the current status of the panel flutter p...
Design factors for flutter control of stiffened exterior skin panels for hypersonic aircraf