Accession Number : AD0754683

Title :   Experimental Research of the Effect of the Angle of Rotation of Stator Blades on the Operation of a Small-Size Turbine Stage,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kurzon,A. G. ; Robinshtein,Yu. V.

Report Date : 10 NOV 1972

Pagination or Media Count : 16

Abstract : The report gives the results of an investigation of three small sized turbine stages with various angles of fixation of the nozzle vanes. Factors are examined which influence the efficiency of the stage during the rotation of the nozzle vanes. A comparison is made with data of similar experiments on stages of large size. (Author)

Descriptors :   (*GAS TURBINES, FUEL CONSUMPTION), TURBINE STATORS, GAS TURBINE NOZZLES, GAS TURBINE BLADES, FLOW FIELDS, NOZZLE AREA RATIO, OPTIMIZATION, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE