Experimental Investigation of the Damping in Roll of Cruciform Triangular Wing-Body Combinations at Mach Numbers from 1.5 to 6.0

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Document Details

Document Type
Technical Report
Publication Date
Apr 07, 1954
Accession Number
AD0029123

Entities

People

  • Alfred G. Boissevain

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Airfoils
  • Aspect Ratio
  • Bodies
  • Boundaries
  • Boundary Layer
  • Delta Wings
  • Equations
  • Flow
  • Free Flight
  • Free Stream
  • Leading Edges
  • Mach Number
  • Measurement
  • Slender Bodies
  • Standards
  • Wind Tunnels