WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEEDS OF A SPOILER-SLOT- DEFLECTOR COMBINATION ON A NACA 65A006 WING WITH QUARTER-CHORD LINE SWEPT BACK 32.6

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Document Details

Document Type
Technical Report
Publication Date
May 29, 1953
Accession Number
AD0011093

Entities

People

  • Raymond D. Vogler

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aluminum Alloys
  • Aspect Ratio
  • Coefficients
  • Deflectors
  • Dynamic Pressure
  • Free Stream
  • Fuselages
  • High Angles
  • Mach Number
  • Reynolds Number
  • Spoilers
  • Static Pressure
  • Surfaces
  • Thick Wings
  • Wind Tunnels