Propulsion System Flow Stability Program (Dynamic). Part VII. Description and Results of a Program for Predicting Performance of a Fan/Compressor with Arbitrary Flow Division.

Abstract

The analytic concept and capabilities of a computer program for predicting performance of a fan/compressor with arbitrary flow division are described in this volume, Part VII. It further presents comparisons of YTF-33 fan/compressor test data with program predictions. Finally, the results of parametric studies to evaluate the effects of the front fan and the splitter lip on the compressor performance at different bypass ratios are presented. It was concluded that the program is a valuable tool for predicting fan/compressor performance at off-design conditions, and for determining modifications that would improve performance. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1970
Accession Number
AD0866554

Entities

People

  • Willem Jansen

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Cognitive Systems Engineering
  • Compressors
  • Computer Programs
  • Computers
  • Cooperation
  • Engineering
  • Interdisciplinary Science
  • Mechanical Engineering
  • Mechatronic Engineering
  • Propulsion Systems
  • Systems Engineering
  • Systems Science

Readers

  • Aerospace Engineering
  • Computer Science.
  • Fluid Mechanics and Fluid Dynamics.