SUPERSONIC FLOW PAST AXIALLY SYMMETRIC BLUNT BODIES WITH A DETACHED SHOCK WAVE

Document Details

Document Type
Technical Report
Publication Date
May 11, 1962
Accession Number
AD0288457

Entities

People

  • F.v. Shugayev

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Blunt Bodies
  • Bodies
  • Flow
  • Shock
  • Shock Waves
  • Supersonic Flow
  • Waves

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow