Accession Number:

AD0851904

Title:

Propulsion System Flow Stability Program (Dynamic). Part IX. Model for Predicting Compressor Performance with Combined Circumferential and Radial Distortion - Computed and Experimental Results.

Descriptive Note:

Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1,

Corporate Author:

NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV

Personal Author(s):

Report Date:

1968-12-01

Pagination or Media Count:

99.0

Abstract:

This report presents the computed results obtained with a computer program designed to predict the performance of a multistage axial compressor operating with combined circumferential and radial distortion it presents comparisons between the computed performance and that experimentally realized on a number of compressor configurations. Author

Subject Categories:

  • Fluid Mechanics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE