EXPERIMENTAL INVESTIGATION OF INTERACTION OF COMPRESSION SHOCKS AND THE BOUNDARY LAYER IN THE RANGE OF MACH NUMBERS BETWEEN = 1.0 AND 1.8,

Document Details

Document Type
Technical Report
Publication Date
Mar 15, 1965
Accession Number
AD0614629

Entities

People

  • G. L. Grodzovskii

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Compression
  • Layers
  • Mach Number
  • Shock
  • Shock Waves
  • Transport Ships