INVESTIGATION AT HIGH SUBSONIC SPEEDS OF SOME EFFECTS OF SIDESLIP ON THE AERODYNAMIC LOADS ON FINNED AND UNFINNED BODIES MOUNTED FROM THE SWEPT-WING OF A WING-FUSELAGE MODEL

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Document Details

Document Type
Technical Report
Publication Date
Apr 26, 1956
Accession Number
AD0092214

Entities

People

  • Thomas J. King Jr.

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aerodynamic Loading
  • Aircrafts
  • Airplanes
  • Dynamic Loads
  • External Stores
  • Fineness Ratio
  • Government Procurement
  • Governments
  • High Angles
  • Mach Number
  • Plastic Explosives
  • Reynolds Number
  • Swept Wings
  • United States Government
  • Wing Tips