Theory of Thin Wing in a Supersonic Flow with Consideration of the Non-Equilibrium State of Excitation of Oscillating Degrees of Freedom,

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Document Details

Document Type
Technical Report
Publication Date
Nov 09, 1978
Accession Number
ADA065992

Entities

People

  • Ye. P. Aksenov
  • Yu. N. Grigor'yev

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • C4I
  • Counter IED
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundaries
  • Discontinuities
  • Equations
  • Excitation
  • Flow
  • Foreign Technology
  • Relaxation Time
  • Shock Waves
  • Specific Heat
  • Supersonic Flow
  • Thin Wings
  • Time Intervals
  • Waves

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight