INVESTIGATION OF DRAG REDUCTION BY BOUNDARY-LAYER SUCTION ON A 36-DEG SWEPT WING AT M = 2.5 TO 4

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1963
Accession Number
AD0297204

Entities

People

  • J.s. Deitering
  • S.r. Pate

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Boundaries
  • Boundary Layer
  • Coefficients
  • Drag
  • Drag Reduction
  • Flow
  • Gas Dynamics
  • Geometry
  • Governments
  • Laminar Flow
  • Layers
  • Mach Number
  • Reynolds Number
  • Suction Slots
  • Swept Wings
  • Wind Tunnels