Supersonic Flow in the Area of Antisymmetric Thin Cruciform Wings with Supersonic Leading Edges in a Horizontal Plane, with Consideration of Flow Separation on the Edges,

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Document Details

Document Type
Technical Report
Publication Date
Oct 30, 1978
Accession Number
ADA065993

Entities

People

  • Stefan Staicu

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Center Of Gravity
  • Coefficients
  • Cruciform Wings
  • Delta Wings
  • Equations
  • Flow
  • Flow Separation
  • Foreign Technology
  • Intensity
  • Leading Edges
  • Perturbations
  • Pressure Distribution
  • Supersonic Flow
  • Thickness
  • Thin Wings

Technology Areas

  • Hypersonics