A thin-layer Navier-Stokes code capable of predicting steady-state viscous flows is applied to the transonic flow over a Space Shuttle configuration. The code is written in the generalized coordinate system, and the grid-generation code of Fujii (1983) is used for the discretization of the flow field. The flow-field computation is done using the CRAY 1S computer at NASA Ames. The computed result is physically reasonable, even though no experimental data is available for the comparison purpose.
Viscous transonic flow computation over Space Shuttle configuration
1984-01-01
Conference paper
No indication
English
Numerical Simulation of Transonic Flow over Space Shuttle Orbiter Tail
British Library Conference Proceedings | 1998
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