ACHIEVEMENT OF VERY HIGH LIFT-DRAG RATIOS AT SUPERSONIC SPEEDS THROUGH DRAG TRANS-FORMATION AND REDUCTION

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1958
Accession Number
AD0150694

Entities

People

  • Roger P. Johnson

Organizations

  • RAND Corporation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Airframes
  • Airplanes
  • Altitude
  • Boundary Layer
  • Flow
  • Jet Aircraft
  • Layers
  • Mach Number
  • Sea Level
  • Skin Friction
  • Supersonic Aircraft
  • United States
  • United States Government
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow