Propulsion System Flow Stability Program (Dynamic). Part IX. Model for Predicting Compressor Performance with Combined Circumferential and Radial Distortion - Computed and Experimental Results.
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1968
- Accession Number
- AD0851904
Entities
People
- R. A. Novak
- R. M. Hearsey