Effect of Bluntness and Angle of Attack on Boundary Layer Transition on Cones and Biconic Configurations,

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1978
Accession Number
ADA064803

Entities

People

  • Kenneth F. Stetson

Organizations

  • Flight Dynamics Laboratory

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Blunt Bodies
  • Bodies
  • Boundary Layer
  • Boundary Layer Transition
  • Coefficients
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Heat Transfer Coefficients
  • Hypersonic Wind Tunnels
  • Laminar Boundary Layer
  • Measurement
  • Reynolds Number
  • Shock Tunnels
  • Test Facilities
  • Wind Tunnels