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Development of a Method which may be Used for Predicting the Inelastic
Acoustic Interaction Problems
5 other sections not shown
acoustic aerodynamic aeroelastic AIAA aircraft amplitude analysis angle angle of attack bending blast wave body shock boundary condition caliber cavitation coefficients component computed configuration coordinate coupling curve cylindrical shell damping dimensionless displacement dynamic pressure effect elastic axis exit experimental finite difference flexural flow field fluid loading flutter speed foil forces free surface geometry Green's function hydrodynamic hydrofoil impact pressure inertia infinite instability integral Lagrange equations linear liquid Mach number mass density ratio mass ratio method missile modal mode shape motion natural frequencies nonlinear normal modes oblique shock obtained oscillation Panel Flutter parameters predicted projectile radiation loading reflected response rigid shadowgraphs shock interaction shock wave shown in Fig simulated solution spherical spheroidal stability static stress strut studies submerged structure supercavitating Supersonic techniques theoretical theory tion torsion two-dimensional vacuo values vector vehicle velocity vibration wavelength wedge wind tunnel zero