Thrust vectoring through fluid injection in an axisymmetrical supersonic nozzle: Theoretical and computational study-Reference-Cited by-同舟云学术

Thrust vectoring through fluid injection in an axisymmetrical supersonic nozzle: Theoretical and computational study

Published:2009 Issue: Volume: Page:1141-1146
ISSN:
Container-title:Shock Waves
language:
Short-container-title:

Author:

Maarouf N.,Sellam M.,Grignon M.,Chpoun A.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-540-85181-3_56.pdf

Reference7 articles.

1. Kenrick A. Waithe and Karen A. Deere, Experimental and computational investigation of multiple injection ports in a convergent-divergent nozzle for fluidic thrust vectoring. AIAA-2003-3802

2. B. Mangin, A. Chpoun, L. Jacquin, Experimental and numerical study of the fluidic thrust vectoring of a two-dimensional supersonic nozzle. Private communication.

3. F. W. Spaid, E. E. Zukoski, A study of the interaction of gaseous jets from transverse slots with supersonic external flows. AIAA journal, Vol. 6, 1968

4. David J. Wing, Victor J. Giuliano, Fluidic Thrust Vectoring of an axisymmetric exhaust nozzle at static conditions. FEDSM97-3228, 1997

5. C. Campbell, J. Farely, Performence of several conical convergent-divergent rocket-type exhaust nozzles. NASA TN D-467, September 1960

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