INVESTIGATION BY THE TRANSONIC-BUMP METHOD OF A 35 deg SWEPTBACK SEMISPAN MODEL EQUIPPED WITH A FLAP OPERATED BY A SERIES OF SERVOVANES LOCATED AHEAD OF AND GEARED TO THE FLAP

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1956
Accession Number
AD0092432

Entities

People

  • Robert F. Thompson
  • William H. Phillips

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Aspect Ratio
  • Boundary Layer
  • Control Sticks
  • Control Surfaces
  • Control Systems
  • Flaps (Control Surfaces)
  • Leading Edges
  • Mach Number
  • Measurement
  • Reynolds Number
  • Surfaces
  • Wind Tunnel Tests
  • Wind Tunnels