Propulsion System Flow Stability Program (Dynamic). Part VIII. Model for Predicting Compressor Performance with Combined Circumferential and Radial Distortion - Computer Program.

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Report Number: AFAPL TR 68-142 Part VIII
Author(s): Novak, R. A., Hearsey, R. M.
Corporate Author(s): Northern Research and Engineering Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1968-12
Pages: 304
Contract: F333615-67-C-1848
DoD Task:
Identifier: AD0851903

The report describes in detail a computer program designed to enable the performance of axial flow compressors operating under asymmetric inlet conditions to be predicted. The underlying theory is given in Part VII; a comparison between results obtained and experimental data is made in Part IX. The report is divided into a number of sections, the principal ones being those giving a Functional Discription of the program, and an Operational Description of the program. The Functional Description is intended to enable the program to be used. The Operational Description of the program is intended to enable the methods used in the program to be understood in detail, hence allowing the program to be modified if desired.

Provenance: Lockheed Martin Missiles & Fire Control

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