SOME MEASUREMENTS OF THE BUFFET REGION OF A SWEPT-WING RESEARCH AIRPLANE DURING FLIGHTS TO SUPERSONIC MACH NUMBERS

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Document Details

Document Type
Technical Report
Publication Date
May 28, 1953
Accession Number
AD0011172

Entities

People

  • Thomas F. Baker

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Airframes
  • Airplanes
  • Altitude
  • Amplitude
  • Flight
  • Frequency
  • High Altitude
  • Intensity
  • Jet Engines
  • Mach Number
  • Measurement
  • Research Aircraft
  • Swept Wings
  • Turbojet Engines

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow