Euler technology assessment program for preliminary aircraft design employing SPLITFLOW code with cartesian unstructured grid method
Euler technology assessment program for preliminary aircraft design employing SPLITFLOW code with cartesian unstructured grid method
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- Washington, D.C. National Aeronautics and Space Adminstration 1995
- 100 p.
- NASA CR 4649 : 1995 .
Computational fluid dynamics, Euler formulation, Preliminary aircraft design, Sharp-edge flow separation, Vortex flow
LNASA CR 4649 : 1995
Computational fluid dynamics, Euler formulation, Preliminary aircraft design, Sharp-edge flow separation, Vortex flow
LNASA CR 4649 : 1995