Application of BCFD Unstructured Grid Solver to Simulation of Micro-ramp Control of Shock/Boundary Layer Interactions
- Author(s):
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Applied Aerodynamics Conference
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-3914
- Paper no.:
- AIAA Paper 2007-3914
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200713 [CD-ROM 2007 Disc 13]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
SIMULATIONS OF AN AEROELASTIC CONTROL SYSTEM FOR SHOCK/BOUNDARY LAYER INTERACTIONS
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
CFD results for shock-boundary layer flow control with micro-ramps at various grid densities
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Simulations of Mesoflap Flow Control for Ramp Oblique Shock/Boundary Layer Interactions.
American Institute of Aeronautics and Astronautics |
9
Technical Paper
A Structured and Hybrid-unstructured Grid Euler and Navier-Stokes Solver for General Geometry
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Numerical Investigation of a Super-Sonic Inlet Using Bleed and Micro-Ramps to Control Shock-Wave/Boundary Layer Interactions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |