Development of a Hybrid RANS-LES All-Speed Algorithm for Liquid Rocket Combustion

Development of a Hybrid RANS-LES All-Speed Algorithm for Liquid Rocket Combustion

Author(s):

S. Thakur ( University of Florida, Gainesville, FL )
J. Wright ( Streamline Numerics Inc., Gainesville, FL )

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-5252

Paper no.:

AIAA 2008-5252

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200808 [CD-ROM 2008 Disc 8]

Type:

Technical Paper

Details

TDL ID:	ZA00050885
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Conf. info. (Number):	44th
Conf. info. (Venue):	Hartford, CT
Conf. info. (Date):	2008.07.21-2008.07.23
Note for article:	44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, 21-23 July 2008

Similar Items:

1 Technical Paper A Rule-Based Algorithm for Liquid Rocket Combustion J. Wright, S. Thakur American Institute of Aeronautics and Astronautics	7 Technical Paper CFD Predictions of Turbomachinery Flows Using Quasi-Steady and Unsteady Models Thakur, S., Wright, J. American Institute of Aeronautics and Astronautics
2 Technical Paper Recent Progress Towards a Rule-Based Computational Tool for Liquid Rocket Combustion E. Luke, S. Thakur, D. Thompson, J. Wright, W. Shyy American Institute of Aeronautics and Astronautics	8 Technical Paper Design of an Optical Port in the Combustion Chamber of a Labscale Hybrid Rocket Motor Meadors, Constance, Elsasser, J.E., Wright, A.B., Hudson, M.K. American Institute of Aeronautics and Astronautics
3 Technical Paper Validation of a New Parallel All-Speed CFD Code in a Rule-Based Framework for Multidisciplinary Applications R. Kamakoti, S. Thakur, J. Wright, W. Shyy American Institute of Aeronautics and Astronautics	9 Technical Paper Effects of Swirling Liquid Oxygen Flow on Combustion of a Hybrid Rocket Engine Kitagawa, K., Mitsutani, T., Ro, T., Yuasa, S. American Institute of Aeronautics and Astronautics
4 Technical Paper A Pressure-Based Algorithm for Reacting Flows with Finite Rate Chemistry Thakur, S., Wright, J., Shyy, W. American Institute of Aeronautics and Astronautics	10 Technical Paper 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
5 Technical Paper An Algorithm for Chemically Reacting Flows on Generalized Grids Using a Rule-Based Framework Thakur, S., Wright, J., Shyy, W. American Institute of Aeronautics and Astronautics	11 Technical Paper A Parallelized, Adaptive, Multi-Grid Hybrid Unstructured Solver for All-Speed Flows. Zhang, S.J., Liu, J., Chen, Y.-S., Godavarty, C.D., Mallapragada, P. American Institute of Aeronautics and Astronautics
6 Technical Paper Conjugate Heat Transfer in a Gas Turbine Blade Trailing-Edge Cavity. Thakur, S., Wright, J. American Institute of Aeronautics and Astronautics	12 Technical Paper Pressure Measurement in the Post-Combustion Section of a Hybrid Rocket Motor Wright, A. B., Tomany, A., Wright, A. M., Hudson, M. K. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12