Drag and Cooling Tests in the 24 ft Wind Tunnel on a Centaurus-Buckingham Wing Nacelle Installation. Part 3. Tests with High Speed Cowl Entry (Tempest Type)

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1946
Accession Number
ADA800693

Entities

People

  • B. Stokes
  • C. Roe
  • H. Shaw
  • T. B. Owen

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Aircrafts
  • Cooling
  • Cooling Fans
  • Diameters
  • Exhaust Pipes
  • Exhaust Systems
  • Fans
  • Flight
  • Flight Speeds
  • Free Stream
  • Measurement
  • Pressure Measurement
  • Propeller Blades
  • Propellers
  • Static Pressure
  • Wind Tunnels