Propulsion System Installation Corrections. Volume 3 Sample Cases

Abstract

This document presents the results from the application of PITAP procedure to two typical aircraft configurations. The two configurations used are the Lightweight Fighter (LWF) and the F-4J. The Lightweight Fighter in the example is a study configuration for which extensive analysis and wind tunnel test data are available for comparison with predicted results. The F-4J is also a configuration that has been extensively tested during the Exhaust System Interaction Program. Data from these tests are used to compare with PITAP predicted results.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1972
Accession Number
AD0907816

Entities

People

  • William H. Ball

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Boundary Layer
  • Computer Programs
  • Computers
  • Diffusers
  • Engineering
  • Exhaust Systems
  • Flow
  • Free Stream
  • Geometry
  • Mach Number
  • Mass Flow
  • Propulsion Systems
  • Subsonic Diffusers
  • Test And Evaluation
  • Wind Tunnels

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