STUDY OF FLOW PAST A CIRCULAR CYLINDER USING A HIGHER ORDER SCHEME FOR NAVIER-STOKES EQUATION
- 著者名:
- Sengupta, T. K. et al. ( National Aeronautical Lab. )
- 掲載資料名:
- NASA Technical Reports(N89)
- 発行年:
- 1988
- 号:
- TM-FM-8806
- 通号:
- G6/34 0161435
- ペーパー番号:
- N89-11142
- 開始ページ:
- 1
- 終了ページ:
- 13
- 総ページ数:
- 13
- 出版情報:
- National Aeronautics and Space Administration
- 言語:
- 英語
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
テクニカルペーパー
Higher-Order Temporal Schemes with Error Controllers for Unsteady Navier-Stokes Equations
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
Higher Order Time Integration Schemes for the Unsteady Navier-Stokes Equations on Unstructured Meshes.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
テクニカルペーパー
Numerical Study of Flow Past a Circular Cylinder Using RANS, Hybrid RANS /LES and PANS Formulations
American Institute of Aeronautics and Astronautics |
4
テクニカルペーパー
ANALYSIS OF TWO-DIMENSIONAL INCOMPRESSIBLE FLOW PAST AIRFOILS USING UNSTEADY NAVIER-STOKES EQUATIONS
National Aeronautics and Space Administration |
10
テクニカルペーパー
Anisotropic Turbulent Flow Simulations Using the Lagrangian Averaged Navier-Stokes-a Equations
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
THE COMPUTATION OF FLOW PAST AN OBLIQUE WING USING THE THIN-LAYER NAVIER-STOKES EQUATIONS
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Calculation of Hypersonic Turbulent Flows Using the Parabolized Navier-Stokes Equations
Society of Automotive Engineering, Inc. |