CFD Results for Shock-Boundary Layer Flow Control with Micro-ramps at Various Grid Densities-Reference-Cited by-同舟云学术

CFD Results for Shock-Boundary Layer Flow Control with Micro-ramps at Various Grid Densities

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA Fluid Dynamics Conference
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Author:

Domel Neal¹,Baruzzini Dan¹,Miller Daniel¹

Affiliation:

1. Lockheed Martin Aeronautics Corp.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4016

Reference7 articles.

1. Anderson, B.H., Tinapple, J., and Surber, L. "Optimal Control of Shock Wave Turbulent Boundary Layer Interactions UsingMicro-ArrayActuation,"AIAA2006-3197.

2. Atkinson, M.D. "Numerical Investigation of a Super-Sonic Inlet Using Bleed and Micro-Ramps to Control Shock-Wave/BoundaryLayer Interactions,"AIAA2007-24.

3. Domel, N.D., and Karman, S.L. "Splitflow: Progress in 3D CFD with Cartesian Omni-tree Grids for Complex Geometries," AIAA2000-1006 WIND CFD - structured Falcon CFD - hybrid - shock added last Fine Shock Fine BL (fixed) Pt/Pt0=.9150 Pt/Pt0=.9016 264K cells 4.9M cells Figure 15: Solution summary - other CFD tools

4. Pitt Ford, C.W., and Babinsky, H. "Micro-Ramp Control for Oblique Shock Wave / BoundaryLayer Interactions," AIAA2007-4115.

5. Shinn, A.F., Vanka, S.P, Mani, M., Dorgan, A., and Michal, T. "Application ofBCFD Unstructured Grid Solver to SimulationofMicro-ramp Control ofShock/BoundaryLayer Interactions,"AIAA2007-3914.

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