Accession Number : AD0700805

Title :   THE OPTIMUM INCIDENT ANGLE ON LOW-ASPECT-RATIO ROTOR BLADES OF A COMPRESSOR STAGE,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kovalevskii,V. V.

Report Date : 09 OCT 1969

Pagination or Media Count : 13

Abstract : Optimal incident angles in rotors with a blade aspect rate of 0.56 and solidity ratios of 1.15 and 1.77 were studied experimentally. A rotor with an aspect ratio of 0.84 and a solidity ratio of 1.18 was also tested.

Descriptors :   (*COMPRESSOR BLADES, CONFIGURATION), (*AXIAL FLOW COMPRESSORS, OPTIMIZATION), ASPECT RATIO, DESIGN, EXPERIMENTAL DATA, VELOCITY, REYNOLDS NUMBER, USSR

Subject Categories : Hydraulic and Pneumatic Equipment

Distribution Statement : APPROVED FOR PUBLIC RELEASE