English

DTIC AD0264140: SYMPOSIUM PROCEEDINGS STRUCTURAL DYNAMICS OF HIGH SPEED FLIGHT, LOS ANGELES, CALIFORNIA - APRIL 24, 25, 26, 1961

Contents: Concepts for aeroelastic system approximations; static aerodynamics for flutter analyses; flutter at high mach numbers; an indicial flutter analysis for hypersonic delta wings; a theory for aeroelastic studies of delta lifting surfaces; flutter of flat panels in a low supersonic flow; flutter of rectangular panels; model flight testing on high-speed tracks; liquid behavior in rocket propellant tanks; dynamics of LP vehicles; aero-inertial control system; dynamic loads of missile configurations; wind loads on a vertically rising vehicle; random gust and taxi response calculations for delta wing aircraft; blast-loading on airfoils; stall buffeting loads; a method for analyzing heated wings; deformational response of heated wing structures; thermal stiffness; acoustic fatigue tests for elevated temperatures structural design; structural vibration in space vehicles; structural response in noise inputs; captive missile response to random pressures; structural response to the noise input of the Saturn engines; the environmental vibration problem.

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