Propulsion System Integration and Test Program (Steady State)-Summary. Part I. Integration Technique and Test Activities.

Abstract

The report describes a propulsion system/airplane integration technique and summarizes the results of six test programs conducted during the study. The six tests were: Thrust diverter/vectoring system flow tests; Shared exit ejector nozzle static tests; Nozzle interaction drag tests; Inlet drag tests; Low speed auxiliary inlet tests; and YTF-33 turbofan engine tests. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1969
Accession Number
AD0856229

Entities

People

  • Robert H. Johnson

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Engines
  • Gas Turbine Nozzles
  • Nozzles
  • Propulsion Systems
  • Static Tests
  • Steady State
  • Turbofan Engines

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.