Wind-Tunnel Investigation of Effects of a Pusher Propeller on Lift, Profile Drag, Pressure Distribution, and Boundary-Layer Transition of a Flapped Wing

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1945
Accession Number
ADA801059

Entities

People

  • Carl A. Sandahl

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Boundaries
  • Boundary Layer
  • Boundary Layer Transition
  • Coefficients
  • Drag
  • Free Stream
  • Layers
  • Leading Edges
  • Load Distribution
  • Pressure Distribution
  • Propellers
  • Slotted Flaps
  • Surfaces
  • Trailing Edges
  • Wind Tunnels