EFFECT OF FOREBODY STRAKES ON THE AERODYNAMIC CHARACTERISTICS IN PITCH AND SIDESLIP OF A HYPERSONIC AIRPLANE CONFIGURATION AT MACH NUMBERS OF 1.41, 2.01, AND 6.86

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1959
Accession Number
AD0312322

Entities

People

  • Cornelius Driver

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aeronautics
  • Aircrafts
  • Airfoils
  • Airframes
  • Airplanes
  • Aspect Ratio
  • Fighter Aircraft
  • Government Procurement
  • Governments
  • Horizontal Stabilizers
  • Leading Edges
  • Mach Number
  • Swept Wings
  • Sweptback Wings
  • Trailing Edges

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow