Experimental Study of Pilot Losses During the Rotation of Supersonic Flow through Wide Angle in Curvilinear Channels,

Document Details

Document Type
Technical Report
Publication Date
Feb 12, 1975
Accession Number
ADA007396

Entities

People

  • I. I. Amarantova
  • V. S. Sadovskii

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Angular Motion
  • Flow
  • Rotation
  • Supersonic Flow
  • Wide Angles

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight