Transonic Euler calculations about a complex multicomponent configuration are presented. The 3D Euler equations are solved utilizing an upwind-biased, alternating direction implicit, approximately factored, multigrid algorithm. Computational results are compared to experimental data of the finned store in a carriage position.
Transonic solutions of a wing/pylon/finned store using hybrid domain decomposition
AIAA Atmospheric Flight Mechanics Conference ; 1992 ; Hilton Head Island, SC, United States
1992-01-01
Conference paper
No indication
English
Nonlinear aeroelastic computations of a wing/pylon/finned-store using parallel computing
Tema Archive | 2005
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