Accession Number : AD0700578

Title :   EFFECT OF THE REYNOLDS NUMBER ON TIP LOSSES,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Maksudyan,A. S. ; Chernikov,V. A.

Report Date : 05 NOV 1969

Pagination or Media Count : 12

Abstract : An examination is made of the effect on the Reynolds number on tip losses in foil lattices and under conditions of a rotating turbine stage. The foil lattices were tested on a static stand, while the stages were tested on an experimental turbine. Careful finishing of the blade surfaces excluded the influence of roughness. (Author)

Descriptors :   (*GAS TURBINE BLADES, *REYNOLDS NUMBER), CASCADE STRUCTURES, EFFICIENCY, FRICTION, ROTATION, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE