CFD simulation of mixing and combustion in LOX/CH4 spray under supercritical conditions

CFD simulation of mixing and combustion in LOX/CH4 spray under supercritical conditions

著者名:

De Giorgi, Maria Grazia ( University of Salento –Dep. Engineering for Innovation , Lecce, Italy, I-73100 )
Leuzzi, Alessio

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Fluid Dynamics Conference

シリーズ巻号:

2009

発行年:

2009

通号:

2009-4038

ペーパー番号:

AIAA Paper 2009-4038

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200907

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00066600
シリーズID:	PA00000147
会議名:	AIAA Fluid Dynamics Conference
回次:	39
会議開催地:	San Antonio, Texas
会議開催年:	2009.06.22-2009.06.25
論文注記:	DOI:10.2514/6.2009-4038 // 39th AIAA Fluid Dynamics Conference 22 - 25 June 2009, San Antonio, Texas

類似資料:

1 テクニカルペーパー Combustion of Lox with H2(g) Under Subcritical, Critical, and Supercritical Conditions (Task1) and Experimental Ovservation of Dense Spray and Mixing of … Kuo, K.K., Hsieh, W.H., Cheung, F.B. National Aeronautics and Space Adminstration	7 テクニカルペーパー Real Gas CFD Simulation of Supercritical H2-LOX in the MASCOTTE Single Injector Combustor Using a Commercial CFD Code M. Poschner, M. Pfitzner American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Simulation of cryogenic cavitation by using both inertial and heat transfer control bubble growth De Giorgi, Maria Grazia, Ficarella, Antonio American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Fundamental Measurements of Multicomponent Turbulent Spray Mixing in Transcritical and Supercritical Conditions Tran, T., Kochar, Y., Seitzman, J., Polikhov, S., Segal, C. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー A CFD Method for Simulation of Mixing and Combustion in High-Pressure LOX/Methane Rocket Engines L. Cutrone, F. Battista, G. Ranuzzi, S. Bonifacio, J. Steelant American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Numerical Simulation of Cryogenic Jets Under Supercritical Conditions. Barata, J., Silva, A., Gokalp, I. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Supercritical High Pressure Combustion Simulation for LOX/CH4 Rocket Propulsion Systems L. Cutrone, F. Battista, G. Ranuzzi American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Mixing and Combustion of Swirl Co-Axial Injectors for Cryogenic Propellants at Supercritical Conditions Zong, N., Yang, V. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Direct Numerical Simulations of O2/ H2 Temporal Mixing Layers Under Supercritical Conditions Okong'o, N., Harstad, K., Bellan, J. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Mixing and Combustion in Supercritical O2/CH4 Liquid Rocket Injectors Ierardo, N., Congiunti, A., Bruno, C. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Spray and Soot Formation Analysis by Means of a Quasi-Dimensional Multizone Model in a Single Cylinder Diesel Engine under Euro 4 Operating Conditions Roberto Finesso, Ezio Spessa, Ezio Mancaruso, Luigi Sequino, Bianca Maria Vaglieco Society of Automotive Engineers	12 テクニカルペーパー A General Platform for the Modeling and Optimization of Conventional and More Electric Aircrafts Teresa Donateo, Maria Grazia De Giorgi, Antonio Ficarella, Elisabetta Argentieri, Elena Rizzo Society of Automotive Engineers

1

2

3

4

5

6

7

8

9

10

11

12