Results from computational analysis of a mixed compression supersonic inlet

Results from computational analysis of a mixed compression supersonic inlet

著者名:

Saunders, J. D. ( NASA Lewis Research Center )
Keith, T. G. ( Ohio Aerospace Inst. )

掲載資料名:

NASA Technical Reports

発行年:

1991

号:

NASA-TM-104475

パート:

NAS 1.15:104475

ペーパー番号:

N92-10976

開始ページ:

1

終了ページ:

18

総ページ数:

18

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:

ZA00001428

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1 テクニカルペーパー The 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet Mizukami, M., Saunders, J. D. National Aeronautics and Space Adminstration	7 テクニカルペーパー Extension of Transonic Flow Computational Concepts in the Analysis of Cavitated Bearings Vijayaraghavan, D., Keith, T.G., Jr., Brewe, D.E. National Aeronautics and Space Adminstration
2 テクニカルペーパー 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet Mizukami, M., Saunders, J.D. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Computational analysis of fluidic compression in supersonic flowfields Haws, Richard G., Noall, Jeff S., Daines, Russell L. American Institute of Aeronautics and Astronautics
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