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Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 3 - Performance of blowing insert configuration no. 1

Authors :
Koch, C. C
Smith, L. H., Jr
Publication Year :
1968
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1968.

Abstract

Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, and performance tests using distorted or undistorted inlet flow

Subjects

Subjects :
Auxiliary Systems

Details

Language :
English
Database :
NASA Technical Reports
Notes :
NAS3-7618
Publication Type :
Report
Accession number :
edsnas.19690006778
Document Type :
Report