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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Comparison of panel flutter results from approximate aerodynamic theory with results from exact inviscid theory and experiment
Two- and three-dimensional plates undergoing limit cycle oscillations in supersonic flow treated by Von Karman large deflection theory and quasi- steady aerodynamic theory
Improved numerical procedure for harmonically deforming lifting surfaces from supersonic kernel function method
Bending-torsional flutter of uniform swept wing with velocity component aerodynamic-strip theory
Two- and three-dimensional plates in high supersonic flow undergoing limit cycle oscillations analyzed, using aerodynamic theory and von Karman large deflection plate theory
Equations of motion for flutter and stability of coaxial elastic circular cylindrical shells between which flows compressible fluid
Flutter stability of cylindrical shell in gas stream and external magnetic field
Improved numerical procedure for harmonically deforming lifting surfaces from supersonic kernel function method
Propeller-rotor whirl flutter and effect of hinged blades and flexible twisted blades
Quasi-steady aerodynamic and von Karman large deflection plate theory equations of nonlinear oscillations of fluttering plate for single mode subsonic and sonic or coupled mode supersonic oscillations
Bending torsional flutter of uniform swept wing with velocity component aerodynamic strip theory
Identical flutter boundaries of multibay and one- bay panels with clamped edges in high and low supersonic regions
Flutter amplitude of stressed panels analyzed in terms of amplification ratios
Stability of equilibrium of nonconservative continuous systems with slight damping
Uniform cantilevered bar subject to eccentric compressive follower force, considering warping rigidity, bending-torsional flutter and stability
Quasi-steady aerodynamic and von Karman large deflection plate theory equations of nonlinear oscillations of fluttering plate for single mode subsonic and sonic or coupled mode supersonic oscillations
Lifting surfaces supersonic-hypersonic flutter at angle of attack determined by shock expansion, Newtonian flow and local flow piston theory