Accession Number : AD0762228

Title :   The Use of Variable Pitch in Alignment Units of a Compressor for Reducing Rotor Vibrations,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Meyerson,I. L. ; Gazaryan,Yu. Kh. ; Gorodetskii,M. E.

Report Date : 06 JUN 1973

Pagination or Media Count : 19

Abstract : The report describes a mathematical analysis of variable pitch compressor rotor blades designed to alleviate vibration.

Descriptors :   (*AXIAL FLOW COMPRESSOR BLADES, VIBRATION), (*GAS TURBINES, *AXIAL FLOW COMPRESSORS), ROTOR BLADES(TURBOMACHINERY), CASCADE STRUCTURES, STRESSES, RESONANT FREQUENCY, DAMPING, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE