Preliminary CFD analysis of the vortex hybrid rocket chamber and nozzle flow field

Preliminary CFD analysis of the vortex hybrid rocket chamber and nozzle flow field

著者名:

Knuth, William J. ( Orbital Technologies Corporation (ORBITECtm) )

Gramer, Daniel J. ( Orbital Technologies Corporation (ORBITECtm) )

Chiaverini, Martin J. ( Orbital Technologies Corporation (ORBITECtm) )

Sauer, J. Arthur ( Orbital Technologies Corporation (ORBITECtm) )

Whitesands, R. Harold ( ERC, Incorporated )

Dill, Richard A. ( ERC, Incorporated )

さらに 1 件

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

シリーズ巻号:

1998

発行年:

1998

通号:

98-3351

ペーパー番号:

98-3351

開始ページ:

1

終了ページ:

12

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050858
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	34th
会議開催地:	Cleveland, OH
会議開催年:	1998.07.13-1998.07.15
論文注記:	34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 13-15, 1998/Cleveland, OH

類似資料:

1 テクニカルペーパー SOLID-FUEL REGRESSION RATE AND COMBUSTION BEHAVIOR OF VORTEX HYBRID ROCKET ENGINES Knuth, William H., Chiaverini, Martin J., Gramer, Daniel J., Sauer, J. Arthur American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Vortex Chamber Flow Field Characterization for Gelled Propellant Combustor Applications Anderson, M.H., Valenzuela, R., Rom, C., Bonazza, R., Chiaverini, M.J. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Experimental investigation of a vortex-driven high-regression rate hybrid rocket engine Knuth, William H., Chiaverini, Martin J., Gramer, Daniel J., Sauer, J. Arthur American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Development of a LOX/RP-1 Vortex Combustion Cold-Wall Thrust Chamber Assembly. Sauer, J.A., Knuth, W.H., Malecki, M.J., Chiaverini, M.J., Hall, C.D. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Solid-fuel regression rate and combustion behavior of vortex hybrid rocket engines Knuth, William H., Chiaverini, Martin J., Gramer, Daniel J., Sauer, J. Arthur American Institute of Aeronautics and Astronautics	9 テクニカルペーパー MARS ISRU CO/O2 HYBRID ENGINE DEVELOPMENT STATUS Rice, Eric E., Chiaverini, Martin J., Clair, Christopher P. St., Knuth, William H., Gustafson, Robert J. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Development and testing of a vortex-driven, high-regression rate hybrid rocket engine Knuth, W., Gramer, D., Chiaverini, M., Sauer, J. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Application of two-phase CFD analysis to the evaluation of asbestos-free insulation in the RSRM Whitesides, R. Harold, Dill, Richard A., Purinton, David C. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Vortex Combustion Chamber Development for Future Liquid Rocket Engine Applications. Chiaverini, M.J., Malecki, M.J., Sauer, J.A., Knuth, W.H. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー SRM Internal Flow Test and Computational Fluid Dynamic Analysis Whitesides, R. Harold, Dill, Richard A., Purinton, David C. National Aeronautics and Space Adminstration
6 テクニカルペーパー Vortex Thrust Chamber Testing and Analysis for O2-H2 Propulsion Applications Chiaverini, M.J., Malecki, M.J., Sauer, J., Knuth, W.H., Gramer, D.J. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Cold Flow Analysis of a Vortex Chamber Engine for Gelled Propellant Combustor Applications Anderson, M., Rom, C., Chiaverini, M. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12