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Accession Number:
AD0691668
Title:
EFFICIENCY OF A LOW-ADMISSION SHROUDLESS SUPERSONIC TURBINE STAGE,
Descriptive Note:
Corporate Author:
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Report Date:
1969-06-04
Pagination or Media Count:
9.0
Abstract:
Experimental studies of the efficiency of a low-admission shroudless supersonic turbine stage are described. The studies were carried out at three different radial clearances and at a 1.8 mm axial clearance. The study results indicate that the efficiency of a supersonic shroudless turbine stage significantly depends on the radial clearance. The effect of the radial clearance is more pronounced in a supersonic engine than a subsonic one. The effect of the radial clearance on the efficiency of a shroudless stage depends on the admission magnitude. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE
