Environmental Temperature and Aircraft Compatibility Studies,

Abstract

A study of both landbased and shipboard tests of the F14A aircraft with the MK7 Jet Blast Deflector to investigate the effect of backflow of jet exhaust on the aircraft being launched and the resulting environmental temperature aft and alongside the JBD. Configuration for shipboard installation and desired mode of operation are recommended. Areas for further effort to achieve improved compatibility are also presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1972
Accession Number
AD0752018

Entities

People

  • G. Gaeman
  • W. Goon

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Backflow
  • Deflectors
  • Flow
  • Fluid Flow
  • Shipboard

Readers

  • Combustion and Flow Dynamics.
  • Explosive Engineering.
  • Systems Analysis and Design