ROCKET-POWERED-MODEL INVESTIGATION OF THE HINGE-MOMENT AND NORMAL-FORCE CHARACTERISTICS OF A HALF-DIAMOND TIP CONTROL ON A 60 deg SWEPTBACK DIAMOND WING BETWEEN MACH NUMBERS OF 0.5 AND 1.3

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Document Details

Document Type
Technical Report
Publication Date
Apr 26, 1954
Accession Number
AD0029200

Entities

People

  • James D. Church

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aspect Ratio
  • Coefficients
  • Control Surfaces
  • Deflection
  • Doppler Radar
  • Dynamic Pressure
  • Errors
  • Flight
  • Free Flight
  • Government Procurement
  • Governments
  • Leading Edges
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Trailing Edges