Euler technology assessment for preliminary aircraft design employing overflow code with muliblock structured-grid method
Euler technology assessment for preliminary aircraft design employing overflow code with muliblock structured-grid method
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- Washington, D.C. National Aeronautics and Space Adminstration 1995
- 66 p.
- NASA CR 4651 : 1995 .
Computational fluid dynamics, Euler formulation,Preliminary aircraft design, Sharp-edge flow-separation, Vortex flow
LNASA CR 4651 : 1995
Computational fluid dynamics, Euler formulation,Preliminary aircraft design, Sharp-edge flow-separation, Vortex flow
LNASA CR 4651 : 1995