Application of a Third Order Upwind Scheme to Viscous Flow over Clean and Iced Wings

Application of a Third Order Upwind Scheme to Viscous Flow over Clean and Iced Wings

著者名:

Bangalore, A. ( Georgia Inst. of Tech. )
Phaengsook, N. ( Georgia Inst. of Tech. )
Sankar, L. N. ( Georgia Inst. of Tech. )

掲載資料名:

NASA Technical Reports

発行年:

1994

巻:

19970006701

号:

NASA-CR-202616

パート:

NAS 1.26:202616

開始ページ:

1

終了ページ:

12

総ページ数:

12

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

類似資料:

1 テクニカルペーパー NUMERICAl STUDY OF THE EFECTS OF ICING ON VISCOUS FLOW OVER WINGS Sankar, L.N. National Aeronautics and Space Adminstration	7 テクニカルペーパー STUDIES OF UNSTEADY VISCOUS FLOWS USING A TWO-EQUATION MODEL OF TURBULENCE Semiannual Status Report, 1 Jan. - 30 Sankar, L.N. et al. National Aeronautics and Space Administration
2 テクニカルペーパー NUMERICAL STUDY OF THE EFFECTS OF ICING ON VISCOUS FLOW OVER WINGS Sankar, L.N. National Aeronautics and Space Adminstration	8 テクニカルペーパー Development of a second order upwind scheme with application to supersonic euler flow Kermani, M.J., Plett, E.G. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Application of Higher Order Spatially Accurate Schemes to Rotors in Hover N. Yeshala, A. Egolf, R. Vasilescu, L. Sankar American Institute of Aeronautics and Astronautics	9 テクニカルペーパー DEVELOPMENT OF ITERATIVE TECHNIQUES FOR THE SOLUTION OF UNSTEADY COMPRESSIBLE VISCOUS FLOWS Hixon, Duane, Sankar, L.N. National Aeronautics and Space Adminstration
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5 テクニカルペーパー Application of a Viscous Flow Methodology to the NREL Phase VI Rotor Xu, G., Sankar, L. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Q3D-Wing: Validation of a Modern Lifting-Line Method for Application to Clean and Iced Wings R. Hindman, N. Crist, B. Williams, X. Chi, Y. Choo, T. Shih American Institute of Aeronautics and Astronautics
6 テクニカルペーパー A Third-Order Multidimensional Upwind Algorithm for Flow Simulations on Unstructured Grids Caraeni, D., Fuchs, L. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Application of High-Order Compact Difference Scheme to Vortical Flow Computation over a Delta and Double-Delta Wings Arasawa, T., Fujii, K., Miyaji, K. American Institute of Aeronautics and Astronautics

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