AN EXPERIMENTAL STUDY AT HIGH SUBSONIC SPEEDS OF SEVERAL TAIL CONFIGURATIONS ON A MODEL WITH AN UNSWEPT WING

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Document Details

Document Type
Technical Report
Publication Date
Apr 04, 1956
Accession Number
AD0092663

Entities

People

  • William C. Sleeman Jr.

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Aspect Ratio
  • Dihedral Angle
  • Directional
  • Geometry
  • Government Procurement
  • Governments
  • High Angles
  • Horizontal Stabilizers
  • Low Angles
  • Mach Number
  • Orientation (Direction)
  • United States Government
  • Wing Body Configurations