An Approximate Method for Calculating Three-Dimensional Inviscid Hypersonic Flow Fields

An Approximate Method for Calculating Three-Dimensional Inviscid Hypersonic Flow Fields

著者名:

Riley, Christopher J. ( Langley Research Center )
DeJarnette, Fred R. ( North Carolina State University )

掲載資料名:

NASA Technical Reports

発行年:

1990

号:

NASA-TP-3018

通号:

H1/34 0280218

パート:

NAS 1.60:3018

ペーパー番号:

N90-27066

開始ページ:

1

終了ページ:

26

総ページ数:

26

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:

ZA00001426

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2 テクニカルペーパー An Engineering Mathod for Interactive Invicid-Boundary Layers in Three-Dimensional Hypersonic Flows Riley, Christopher J. National Aeronautics and Space Adminstration	8 テクニカルペーパー Aeroheating Predictions for X-34 Using an Inviscid-Boundary Layer Method Riley, Christopher J., Kleb, William L., Alter, Steven J. National Aeronautics and Space Adminstration
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5 テクニカルペーパー Improved Approximate Method for Computing Convective Heating on Hypersonic Vehicles Using Unstructured Grids H. Hamilton, J. Weilmuenster, F. DeJarnette American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Three-dimensional flow field measurements in a transonic turbine cascade Giel, P. W., Thurman, D. R., Lopez, I., Boyle, R. J., Fossen, G. J. Van The American Society of Mechanical Engineers
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