Study of Heat Transfer in a Gaseous Hydrogen Liquid Oxygen Multi-Element Combustor

Study of Heat Transfer in a Gaseous Hydrogen Liquid Oxygen Multi-Element Combustor

Author(s):

L. Droppers ( Purdue University, West Lafayette, IN )
R. Schuff
W. Anderson

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-5550

Paper no.:

AIAA Paper 2007-5550

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200717 [CD-ROM 2007 Disc 17]

Type:

Technical Paper

Details

TDL ID:	ZA00049509
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	43rd
Conf. info. (Venue):	Cincinnati, OH
Conf. info. (Date):	2007.07.08-2007.07.11
Note for article:	43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, July 8-11, 2007

Similar Items:

1 Technical Paper Measurement and Analysis of Heat Transfer in a Multi-Element Hydrogen/Oxygen Rocket Combustor M. deRidder, D. Helderman, N. Nugent, W. Anderson American Institute of Aeronautics and Astronautics	7 Technical Paper Effects of buoyancy on heat transfer and oxygen consumption in fuel-thermal-stability studies Katta, Viswanath R., Blust, James W., Williams, Theodore F., Martel, Charles R. The American Society of Mechanical Engineers
2 Technical Paper Liquid Film Cooling Using Swirl in Rocket Combustors Yu, Y., Schuff, R., Anderson, W. American Institute of Aeronautics and Astronautics	8 Technical Paper The Effects of Reynolds Number, Rotor Incidence Angle and Surface Roughness on the Heat Transfer Distribution in a Large-Scale Turbine Rotor Passage Blair, M.F., Anderson, O.L., Paterson, R.W. National Aeronautics and Space Adminstration
3 Technical Paper Detailed Flowfield Predictions of Heat Transfer to Supercritical Fluids in High Aspect Ratio Cooling Channels H. Jung, C. Merkle, R. Schuff, W. Anderson American Institute of Aeronautics and Astronautics	9 Technical Paper Computational Modeling of Instabilities in a Single-Element Rocket Combustor Using a Response Function R. Smith, G. Xia, W. Anderson, C. Merkle, V. Sankaran American Institute of Aeronautics and Astronautics
4 Technical Paper Combustion Instability Studies Using Gaseous Methane and Liquid Oxygen W. Marshall, S. Pal, R. Woodward, R. Santoro American Institute of Aeronautics and Astronautics	10 Technical Paper Computational Simulations of the Effect of Chamber Diameter on Single-Element Rocket Combustor Instability G. Xia, R. Smith, W. Anderson, C. Merkle American Institute of Aeronautics and Astronautics
5 Technical Paper Study of Simulated Fuel Flows in High Aspect Ratio Cooling Channels J. Wennerberg, H. Jung, R. Schuff, W. Anderson, C. Merkle American Institute of Aeronautics and Astronautics	11 Technical Paper Characterization of Gas-Centered Swirl-Coaxial Injector Stability in a Subscale Multi-Element Combustor B. Pomeroy, J. Sisco, J. Eckstein, W. Anderson American Institute of Aeronautics and Astronautics
6 Technical Paper A comparative study of the effects of liquid- versus gaseous-oxygen injection on combustion stability in 11-inch-diameter hybrid motors Boardman, T.A., Carpenter, R.L., Claflin, S.E. American Institute of Aeronautics and Astronautics	12 Technical Paper Experimental Investigation of Asymmetric Heating in a High Aspect Ratio Cooling Channel with Supercritical Nitrogen R. Schuff, H. Jung, C. Merkle, W. Anderson American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12