Accession Number:

AD0757217

Title:

The Low Hub-Tip Ratio Supersonic Axial-Flow Compressor. Volume II.

Descriptive Note:

Final rept. 1 Jul 71-30 Jun 72,

Corporate Author:

VON KARMAN INST FOR FLUID DYNAMICS RHODE-SAINT-GENESE (BELGIUM) TURBOMACHINERY LAB

Personal Author(s):

Report Date:

1972-11-01

Pagination or Media Count:

72.0

Abstract:

The report describes the test results of a supersonic axial-flow compressor stage with a tip Mach number of 2.0. This volume discusses a method to eliminate the inlet problem. Author

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE