Accession Number:

AD0688888

Title:

COMPUTATION OF THE LAMINAR COMPRESSIBLE BOUNDARY LAYER.

Descriptive Note:

Final rept. 15 Jun 64-15 Jun 69,

Corporate Author:

STANFORD UNIV CALIF DEPT OF APPLIED MECHANICS

Personal Author(s):

Report Date:

1969-01-01

Pagination or Media Count:

17.0

Abstract:

The report contains abstracts of significant research papers developed on the laminar compressible boundary layer in the stagnation-point region for an axisymmetric blunt body, second-order boundary layer effects in hypersonic flow past axisymmetric blunt bodies, two-dimensional hypersonic stagnation flow at low Reynolds numbers, and a numerical solution for the laminar wake behind a finite flat plate. Author

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE