Propulsion System Flow Stability Program (Dynamic). Part VIII. User's Manual for a Program for Predicting Performance of a Fan/Compressor with Arbitrary Flow Division.

Abstract

This volume, Part VIII of ten parts, contains detailed instructions for operation of the computer program described in Part VII of this report. The program computes performance for a fan/compressor for any specified bypass ratio. Program subroutine listings and example runs are also presented. Some results of the program and comparisons of program predictions with test data which are summarized in Part VII are discussed in greater detail in this volume. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1970
Accession Number
AD0866499

Entities

People

  • A. M. Kirschner
  • S. N. Thirumalaisamy

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Compressors
  • Computer Programs
  • Computers
  • Cooperation
  • Engineering
  • Instructions
  • Procedures (Computers)
  • Propulsion Systems
  • Systems Engineering

Readers

  • Aerospace Engineering
  • Computer Science.