A SHOCK WAVE CAPABILITY FOR THE IMPROVED TWO-DIMENSIONAL KINETICS (TDK)

A SHOCK WAVE CAPABILITY FOR THE IMPROVED TWO-DIMENSIONAL KINETICS (TDK)

著者名:

Nickerson, Gary R. ( Software and Engineering Associates, Inc. )
Dang, Lanh D. ( Software and Engineering Associates, Inc. )

掲載資料名:

NASA Technical Reports

発行年:

1984

号:

NASA-CR-171302

通号:

G3/34 14209

パート:

NAS 1.26:171302

ペーパー番号:

N85-19360

開始ページ:

1

終了ページ:

119

総ページ数:

119

出版情報:

National Aeronautics and Space Administration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:

ZA00002949

類似資料:

1 テクニカルペーパー ENGINEERING AND PROGRAMMING MANUAL: TWO-DIMENSIONAL KINETIC REFERENCE COMPUTER PROGRAM (TDK) Final Report Nickerson, G.R. National Aeronautics and Space Administration	7 テクニカルペーパー A DOCUMENTATION OF TWO- AND THREE-DIMENSIONAL SHOCK-SEPARATED TURBULENT BOUNDARY LAYERS Brown, J. D. et al. National Aeronautics and Space Administration
2 テクニカルペーパー IMPROVED 2-DIMENSIONAL-KINETICS COMPUTER PROGRAM Quarterly Progress Report. 1 Apr.-30 Jun. 1984 Nickerson, G.R. National Aeronautics and Space Administration	8 テクニカルペーパー Numerical simulation of a three-dimensional flame/shock wave interaction Roy, Christopher J., Edwards, Jack R. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Physical analysis of the two-dimensional compressible vortex-shock interaction Kao, C.T., Ellenrieder, K. von, MacCormack, R.W., Bershader, D. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー CONTRIBUTION TO THE OPTIMAL SHAPE DESIGN OF TWO-DIMENSIONAL INTERNAL FLOW WITH EMBEDDED SHOCKS Iollo, Angelo., Salas, Manuel D. National Aeronautics and Space Adminstration
4 テクニカルペーパー Unsteady behavior of the shock wave passing over two and three dimensional obstacles Miyaji, Koji, Fujii, Kozo American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Static Internal Performance of a Two-Dimensional Convergent Nozzle With Thrust-Vectoring Capability up to 60 Leavitt, Laurence D. National Aeronautics and Space Administration
5 テクニカルペーパー Oscillation of Oblique Shock Waves Generated in a Two Dimensional Asymmetric Nozzle Higashino,Fumio, Matsuo,Shigeru, Tsuyuki,Taro Society of Automotive Engineering, Inc.	11 テクニカルペーパー DOCUMENTATION OF TWO- AND THREE-DIMENSIONAL HYPERSONIC SHOCK WAVE/TURBULENT BOUNDARY LAYER INTERACTION FLOWS Kussoy, Marvin I. et al. National Aeronautics and Space Administration
6 テクニカルペーパー Two-dimensional shock-sound interaction on unstructured meshes Stanescu, D., Habashi, W.G. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Shock-induced detonation wave driver for enhancing shock tube performance Stuessy, W.S., Lu, F.K., Wilson, D.R. American Institute of Aeronautics and Astronautics

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