Accession Number : AD0655382
Title : STRENGTH AND DYNAMICS OF AVIATION MOTORS: SELECTED ARTICLES.
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Report Date : 18 APR 1967
Pagination or Media Count : 117
Abstract : Contents: Analysis of conditions of appearance of natural oscillations of a system with one degree of freedom; Curving-twisting oscillations of twisted compressor blades; Conditions of activation of stall flutter of compressor blades.
Descriptors : (*COMPRESSOR BLADES, OSCILLATION), USSR, AIRCRAFT ENGINES, AXIAL FLOW COMPRESSOR BLADES, FLUTTER, VIBRATION, ANGLE OF ATTACK, FORCE(MECHANICS)
Subject Categories : Hydraulic and Pneumatic Equipment
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE