Experiences at the NASA Langley Research Center generating grids about a cranked wing fighter aircraft configuration is described. A single block planar grid about the fuselage and canard used with a finite difference Navier-Stokes solver is also described. A dual block nonplanar grid about the complete configuration and used with a finite volume Euler solver is presented. The very important aspect of computing the aircraft surface grid, starting with a standardized model description, is also presented.
Grid generation on and about a cranked-wing fighter aircraft configuration
1988-03-01
Miscellaneous
No indication
English
Shock-wave patterns on cranked-wing configuration
Engineering Index Backfile | 1960
|Shock-Wave Patterns on a Cranked-Wing Configuration
NTIS | 1960
|The Shock-Wave Patterns on a Cranked-Wing Configuration
NTRS | 1960
|The shock-wave patterns on a cranked-wing configuration
TIBKAT | 1960
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