The goal of this work is to enable the computation of large numbers of unsteady high-fidelity flow simulations for a YAV-8B Harrier aircraft in ground effect by improving the solution process and taking advantage of NASA parallel supercomputers. The YAV-8B Harrier aircraft can take off and land vertically, or utilize short runways by directing its four exhaust nozzles toward the ground. Transition to forward flight is achieved by rotating these nozzles into a horizontal position.
Parametric Powered-Lift Navier-Stokes Computations
2002-06-01
Miscellaneous
No indication
English
Parametric Powered-Lift Navier-Stokes Computations
NTIS | 2004
|Navier-Stokes computations for exotic airfoils
NTRS | 1986
|Wind Tunnel Experiments and Navier-Stokes Computations of a High-Lift Military Airfoil
British Library Conference Proceedings | 1999
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