TRANSONIC WIND-TUNNEL INVESTIGATION OF THE EFFECTS OF A HEATED PROPULSIVE JET ON THE PRESSURE DISTRIBUTION ALONG A FUSELAGE OVERHANG

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Document Details

Document Type
Technical Report
Publication Date
Apr 04, 1956
Accession Number
AD0092794

Entities

People

  • Donald H. Ward
  • Elden S. Cornette

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Afterbodies
  • Bodies
  • Combustion
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Geometry
  • Government Procurement
  • Governments
  • Jet Engines
  • Mach Number
  • Pressure Distribution
  • Static Pressure
  • Transonic Wind Tunnels
  • United States Government
  • Wind Tunnels