Accession Number:

AD0849532

Title:

Heat Transfer in Shock Wave-Boundary Layer Interaction Regions

Descriptive Note:

Technical publication

Corporate Author:

NAVAL WEAPONS CENTER CHINA LAKE CA

Personal Author(s):

Report Date:

1968-11-01

Pagination or Media Count:

89.0

Abstract:

An investigation of the effect of shock wave-boundary layer interaction on aerodynamic heat-transfer coefficients is reported. A literature survey and empirical expressions for predicting peak heat-transfer coefficients in interaction regions, developed with the use of existing experimental data, are presented.

Subject Categories:

  • Guided Missiles
  • Fluid Mechanics
  • Thermodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE