Experimental Flow Investigation of a Truncated Ideal Contour Nozzle

Experimental Flow Investigation of a Truncated Ideal Contour Nozzle

Author(s):

R. Stark ( DLR German Aerospace Research Center, Lampoldshausen, Baden-Wuerttemberg, Germany )
B. Wagner ( University of Stuttgart, Stuttgart, Germany )

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-5208

Paper no.:

AIAA Paper 2006-5208

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200616 [CD-ROM 2006 Disc 16]

Type:

Technical Paper

Details

TDL ID:	ZA00047242
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	42nd
Conf. info. (Venue):	Sacramento, California
Conf. info. (Date):	2006.07.09-2006.07.12

Similar Items:

1 Technical Paper Unsteady Numerical Simulations of the Flow in a Truncated Ideal Contour Nozzle Under Free Shock Separation Conditions Perigo, D., Schwane, R., Wong, H. American Institute of Aeronautics and Astronautics	7 Technical Paper Flow Separation and Side-load Behavior of Truncated Ideal Rocket Nozzles Terhardt,M., Hagemann,G., Frey,M. American Institute of Aeronautics and Astronautics
2 Technical Paper Flow Separation Studies in a Subscale Truncated Ideal Contour Nozzle S. Verma, O. Haidn American Institute of Aeronautics and Astronautics	8 Technical Paper Experimental Investigation of the Acoustics of an Annular Aerospike Nozzle Flow Karthikeyan, N, Verma, S B, Venkatakrishnan, L American Institute of Aeronautics and Astronautics
3 Technical Paper Simulation of Unsteady Three Dimensional Separation Behaviour in Truncated Ideal Contour Nozzles Perigo, D., Schwane, R. American Institute of Aeronautics and Astronautics	9 Technical Paper Flow Separation Phenomena in Subscale Rocket Nozzles. Kwan, W., Stark, R. American Institute of Aeronautics and Astronautics
4 Technical Paper Advanced Flow Visualisation Techniques in Cold Gas Subscale Nozzles, a Comparison Stark, R., Kronmuller, H., Zerjeski, D., Wagner, B. American Institute of Aeronautics and Astronautics	10 Technical Paper Experimental Investigation of Shock-Cell Noise Reduction for Dual-Stream Nozzles in Simulated Flight Janardan, B. A., Yamamoto, K., Majjigi, R. K. National Aeronautics and Space Administration
5 Technical Paper Experimental and Numerical Investigation of Heat Loads in Separated Nozzle Flow Gross,A., Haidn,O., Stark,R., Zeiss,W., Weber,C., Weiland,C. American Institute of Aeronautics and Astronautics	11 Technical Paper Experimental investigation of the flow field in a multistage axial flow compressor Lakshminarayana, B., Suryavamshi, N., Prato, J., Moritz, R. The American Society of Mechanical Engineers
6 Technical Paper Flow Separation in Rocket Nozzles, a Simple Criteria Stark, R. American Institute of Aeronautics and Astronautics	12 Technical Paper Experimental Investigation of Shock-Cell Noise Reduction for Single Stream Nozzles in Simulated Flight Yamamoto, K., Balsa, T. F., Janardan, B. A., knott, P. R. National Aeronautics and Space Administration

1

2

3

4

5

6

7

8

9

10

11

12