Accession Number : ADA951865

Title :   Interaction Region in the Boundary Layer of a Shock Tube.

Descriptive Note : Scientific interim rept.,

Corporate Author : CASE INST OF TECH CLEVELAND OHIO FLUID THERMAL AND AEROSPACE SCIENCES

Personal Author(s) : Ban,Stephen D.

Report Date : JUN 1967

Pagination or Media Count : 146

Descriptors :   *Boundary layer, *Shock tubes, *Mathematical models, Boundary layer flow, Velocity, Temperature, Shock waves

Subject Categories : Numerical Mathematics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE