EFFECT OF FUSELAGE AIR BRAKES ON THE LONGITUDINAL STABILITY CHARACTERISTICS OF A SWEPT-WING FIGHTER MODEL AT TRANSONIC SPEEDS

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Document Details

Document Type
Technical Report
Publication Date
Apr 24, 1956
Accession Number
AD0092443

Entities

People

  • Donald D. Arabian

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Dynamic Pressure
  • Free Stream
  • Government Procurement
  • Governments
  • Leading Edges
  • Mach Number
  • Measurement
  • National Security
  • Pneumatic Brakes
  • Pressure Distribution
  • Pressure Measurement
  • Static Pressure
  • Swept Wings
  • Trailing Edges
  • United States Government