ATTENUATION IN A SHOCK TUBE DUE TO UNSTEADY-BOUNDARY-LAYER ACTION

Document Details

Document Type
Technical Report
Publication Date
Apr 24, 1956
Accession Number
AD0158942

Entities

People

  • Harold Mireis

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Attenuation
  • Boundaries
  • Boundary Layer
  • Layers
  • Shock Tubes
  • Tubes