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) : Novak, R. A. ; Hearsey, R. M.

Report Date : DEC 1968

Pagination or Media Count : 99

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)

Descriptors :   (*TURBOFAN ENGINES, AXIAL FLOW COMPRESSORS), (*AXIAL FLOW COMPRESSORS, AERODYNAMIC CHARACTERISTICS), (*TURBOJET INLETS, FLOW SEPARATION), MATHEMATICAL MODELS, COMPUTER PROGRAMS, PERFORMANCE(ENGINEERING), DISTORTION, STABILITY, PREDICTIONS, ENGINE SURGE, GAS FLOW, AIRCRAFT ENGINES, GAS TURBINES.

Subject Categories : Fluid Mechanics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE