Computational study of a turbulent delta-wing flowfield using two-equation turbulence models | 東京工業大学附属図書館文献データベース

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Computational study of a turbulent delta-wing flowfield using two-equation turbulence models

著者名:: Gordnier, R.E. ( Wright Laboratory, Wright-Patterson AFB )
掲載資料名:: AIAA paper
シリーズ名:: AIAA Paper : AIAA Fluid Dynamics Conference
シリーズ巻号:: 1996
発行年:: 1996
通号:: 96-2076
ペーパー番号:: 96-2076
開始ページ:: 1
終了ページ:: 16
出版情報:: American Institute of Aeronautics and Astronautics
ISSN:: 01463705
言語:: 英語
請求記号:: A07400
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:	ZA00050836
シリーズID:	PA00000147
会議名:	AIAA Fluid Dynamics Conference
回次:	27th
会議開催地:	New Orleans, LA
会議開催年:	1996.06.17-1996.06.20
論文注記:	27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA

類似資料:

1 テクニカルペーパー Computation of Limit Cycle Oscillations of a Delta Wing Gordnier, R. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー On the assessment of one- and two-equation turbulence models for the computation of impinging jet flowfields Ladd, J.A., Korakianitis, T. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー High-Order Simulation of Low Sweep Delta Wing Flows Using a Hybrid RANS/ILES Model R. Gordnier, M. Visbal American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Computation of Turbulent Flow over Highly Curved Configuration Using a Conventional Two-Equation Turbulence Model M. Zakyani, M. Taeibi-Rahni American Institute of Aeronautics and Astronautics
3 テクニカルペーパー TRANSONIC FLOW SOLUTIONS USING A COMPOSITE VELOCITY PROCEDURE FOR POTENTIAL, EULER AND RNS EQUATIONS Gordnier, R.E. et al. National Aeronautics and Space Administration	9 テクニカルペーパー A number study of reacting flow inside combustors using a two-equation model of turbulence and an eddy-dissipation model of turbulent chemistry Lee, J., Fricker, D. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Computational and Experimental Investigation of a Nonslender Delta Wing R. Gordnier, M. Visbal, I. Gursul, Z. Wang American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Computational study of high-angle-of-attack missile flows using two-equation turbulence models Josyula, Eswar American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Some Computational Aeroelastic Results for a Low Sweep Delta Wing at High Angle of Attack (Invited) P. Attar, R. Gordnier American Institute of Aeronautics and Astronautics	11 テクニカルペーパー High Fidelity Computational Simulation of a Membrane Wing Airfoil R. Gordnier American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Higher-Order Compact Difference Scheme Applied to the Simulation of a Low Sweep Delta Wing Flow. Gordnier, R.E., Visbal, M.R. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Unsteady viscous flow computations using a two-equation turbulence model with wall functions Suhs, N.E., Nichols, R.H., Denny, A.G. American Institute of Aeronautics and Astronautics

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