Computation of Three-Dimensional Aerodynamic Flow.
Final rept. 1 Jul 70-30 Jun 76,
MARTIN MARIETTA LABS BALTIMORE MD
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This contract extended from July 1, 1970 to June 30, 1976. The purpose was to calculate numerically three-dimensional laminar boundary layers. During the contracting years, steady progress was made on this very difficult problem, for which there was initially only a minimal foundation. As a result, the basic mathematical problem has now been clarified and numerical methods and computational procedures established. Complete solutions revealed, for the first time, basic three-dimensional boundary layer structure in all details while new separation concepts were discovered. A series of journal publications and technical reports resulted.
- Fluid Mechanics