Exhaust System Interaction Program

Abstract

The program consisted of two phases. The purpose of Phase 1 was to define what needs to be known, and when, and with what accuracy to define the engine cycle and thrust required by a proposed airplane, and to develop methods to obtain the required information -- particularly in the engine-exhaust system area. The second phase simulated the preliminary design and engine airframe matching portions of an airplane system development, stressing the evaluation of exhaust system installation losses at several levels of validity. This final report presents a summary of the work. The individual tasks are documented in seven volumes from Phase 1 (Vols. 1 - 7), ten volumes from Phase 1 (Vols. 8 - 17) of Ancilliary Reports (including D162-10467-12).

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1973
Accession Number
AD0769086

Entities

People

  • John E. Postlewaite
  • Victor Salemann

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computers
  • Contracts
  • Drag
  • Geometry
  • Horizontal Stabilizers
  • Military Aircraft
  • Pressure Distribution
  • Test And Evaluation
  • Turbines
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Business Analytics