A k-e Calculation of Transitional Boundary Layers
- Author(s):
- Yang, Z. ( National Aeronautics and Space Administration Lewis Research Center )
- Shih, T.H.
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1992
- Issue:
- NASA-TM-105604
- Pt.:
- NAS 1.15:105604
- Paper no.:
- N92-22398
- Page(from):
- 1
- Page(to):
- 12
- Pages:
- 12
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
8
Technical Paper
Bypass transitional flow calculations using a Navier-Stokes solver and two-equation models
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Reynolds Stress Calculations for Pre-Transition Boundary Layers with Turbulent Free Streams.
American Society of Mechanical Engineers |
4
Technical Paper
Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
An Improved k- Model for Near-Wall Turbulence and Comparison With Direct Numerical Simulation
National Aeronautics and Space Adminstration |
6
Technical Paper
Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |