Accession Number : AD0614943

Title :   PROBLEMS OF PLATE FLUTTER IN NONLINEAR ARRANGEMENT,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Stepanov,R. D.

Report Date : 15 APR 1965

Pagination or Media Count : 15

Abstract : Results are given of numerical integration of a system of nonlinear differential equations of autooscillation of a plate with consideration of factors, characterizing the geometric and aerodynamic nonlinearity.

Descriptors :   (*FLUTTER, FLAT PLATE MODELS), (*AEROELASTICITY, FLUTTER), SUPERSONIC FLOW, BOUNDARY LAYER, DEFORMATION, DIFFERENTIAL EQUATIONS, OSCILLATION, USSR

Distribution Statement : APPROVED FOR PUBLIC RELEASE