Application of a Navier-Stokes Solver to the Analysis of Multielement Airfoils and Wings Using Multizonal Grid Techniques

Application of a Navier-Stokes Solver to the Analysis of Multielement Airfoils and Wings Using Multizonal Grid Techniques

著者名:

Jones, Kenneth M. ( NASA Langley Research Center )
Biedron, Robert T. ( Analytical Services and Materials )
Whitlock, Mark ( Stanford Univ. )

掲載資料名:

NASA Technical Reports

発行年:

1997

巻:

19970013280

号:

NASA-TM-112005

パート:

NAS 1.15:112005

開始ページ:

1

終了ページ:

28

総ページ数:

28

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:

ZA00001434

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2 テクニカルペーパー Multiblock grid generation process for complex configuration analysis using Navier-Stokes solvers Yu, N.J., Su, T.Y., Wilkinson, W.M. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Prediction of Transonic Buffet Onset for an Airfoil with Shock Induced Separation Bubble Using Steady Navier-Stokes Solver Chung, I., Reu, T., Lee, D. American Institute of Aeronautics and Astronautics
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