EFFECT OF LEADING-EDGE CHORD-EXTENSIONS ON THE AERODYNAMIC CHARACTERISTICS OF A 45 SWEPTBACK WING-FUSELAGE COMBINATION AT MACH NUMBERS OF 0.40 TO 1.03

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Document Details

Document Type
Technical Report
Publication Date
Apr 14, 1953
Accession Number
AD0006725

Entities

People

  • F. E. West Jr.
  • George Liner
  • Gladys S. Martz

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Airfoils
  • Base Pressure
  • Drag
  • Flow
  • Flow Separation
  • Free Stream
  • High Angles
  • High Lift
  • Leading Edges
  • Mach Number
  • Measurement
  • National Security
  • Pressure Distribution
  • Sweptback Wings