Challenge for Natural Transition Simulation of Wing Boundary Layer with an Innovative 3-D LES Technique
- Author(s):
- T. Atobe ( Japan Aerospace Exploration Agency, Chofu, Japan )
- T. Kurotaki
- T. Sumi
- S. Takagi
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Fluid Dynamics Conference
- Ser. no.:
- 2006
- Pub. Year:
- 2006
- No.:
- 2006-3533
- Paper no.:
- AIAA Paper 2006-3533
- Pub. info.:
- Reston, Va: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200611 [CD-ROM 2006 Disc 11]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Numerical Simulation around Airfoil with Natural Transition in High Reynolds Numbers
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Transition Prediction of Three-Dimensional Boundary Layers Using a Complex Ray Theory
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Comparison of Methods for Determining Boundary Layer Edge Conditions for Transition Correlations
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Comparison of Boundary Layer Transition Measurement Techniques on a Laminar Flow Wing
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Large-eddy simulation of laminar-turbulent transition in a swept-wing boundary layer
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Rebirth of Turbulence in Laminarized Boundary Layers along the Wind-Tunnel Contraction
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Evaluation of an innovative supersonic boundary layer transition device - phase 1 results
American Institute of Aeronautics and Astronautics |