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Showing 1 to 6 of 6 for “"Panel Flutter"”.
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Nonlinear panel flutter and its interaction with forcing excitations.
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1972.
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Flutter of rectangular simply supported panels at high supersonic speeds
The panel flutter analysis presented herein has been restricted to the problem of an isolated simply supported plate of uniform thickness. The same type of analysis can be applied, however, to other panel configurations. Clamped panels, integrally stiffened panels, arrays of panels, end others …
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Exploratory Study on the Design of Combined Aero-Thermo-Structural Experiments in High Speed Flows
… potential configurations and responses of panels for experimental tests investigating fluid-thermal-structural interactions. The United States Department of Defense (DoD) and the National Aeronautics and Space Administration (NASA) are both interested in hypersonic vehicles due to their …
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Flutter of sandwich panels at supersonic speeds
Panel flutter is an important design consideration for vehicles traveling at supersonic speeds. Most theoretical analyses of panel flutter consider the motion of the panel to be described adequately by classical thin plate theory. In such a theory, transverse shear deformations are neglected which …
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Nonlinear flutter of composite shear-deformable panels in a high-supersonic flow
… of a laterally compressed, flat, composite panel subjected to a high supersonic flow is analyzed. The structural model considers a higher-order shear deformation theory which also includes the effect of the transverse normal stress and satisfies the traction-free condition on both faces of …
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Aero-servo-viscoelasticity theory: lifting surfaces, plates, velocity transients, flutter, and instability
… considered, either a lifting surface or a panel, and the type of dynamic stability present. For both types of structures, the governing equations are integral-partial differential equations. The spatial component of the governing equations is eliminated using a series expansion of basis …