SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE 2-A DEVELOPMENT PROGRAM. VOLUME 2

Abstract

Pratt & Whitney Aircraft has conducted static (internal flow only) and wind tunnel (internal and external flow) tests of scale models of the engine exhaust system, including thrust reverser, directed toward verification of the exhaust system performance.

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Document Details

Document Type
Technical Report
Publication Date
May 05, 1965
Accession Number
AD0380821

Entities

People

  • R.l. Toft

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Engineers
  • Failure Mode And Effect Analysis
  • Heat Transfer
  • Hybrid Power
  • Jet Aircraft
  • Jet Engine Fuels
  • Jet Engine Noise
  • Materials Science
  • Materials Testing
  • Measurement
  • Mechanics
  • Supersonic Aircraft
  • Supersonic Transport Aircraft
  • Tensile Strength
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Aerospace Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow