INVESTIGATION AT ZERO FORWARD SPEED OF A LEADING-EDGE SLAT AS A LONGITUDINAL CONTROL DEVICE FOR VERTICALLY RISING AIRPLANES THAT UTILIZE THE REDIRECTED-SLIPSTREAM PRINCIPLE

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1956
Accession Number
AD0093389

Entities

People

  • Richard E. Kuhn

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Airplanes
  • Aluminum Alloys
  • Center Of Gravity
  • Control Surfaces
  • Deflection
  • Diameters
  • Flight
  • Government Procurement
  • Governments
  • Ground Effect
  • Leading Edges
  • Slotted Flaps
  • Surfaces
  • Trailing Edges
  • Wind Tunnels