COMPARISON OF EXPERIMENTAL WITH CALCULATED RESULTS FOR THE LIFTING EFFECTIVENESS OF A FLEXIBLE 45 DEG SWEPTBACK WING OF ASPECT RATIO 6.0 AT MACH NUMBERS FROM 0.8 TO 1.3

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Document Details

Document Type
Technical Report
Publication Date
Apr 15, 1954
Accession Number
AD0028961

Entities

People

  • Richard E. Walters

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aircrafts
  • Airframes
  • Aluminum Alloys
  • Aspect Ratio
  • Dynamic Pressure
  • Equations
  • Free Stream
  • Government Procurement
  • Lifting Surfaces
  • Load Distribution
  • Mach Number
  • Measurement
  • Simultaneous Equations
  • Sweptback Wings