COMPUTATION OF THE LAMINAR COMPRESSIBLE BOUNDARY LAYER.
Final rept. 15 Jun 64-15 Jun 69,
STANFORD UNIV CALIF DEPT OF APPLIED MECHANICS
Pagination or Media Count:
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
- Fluid Mechanics