Thrust shock vector control of an axisymmetric conical supersonic nozzle via secondary transverse gas injection

Author:

Zmijanovic V.,Lago V.,Sellam M.,Chpoun A.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Reference27 articles.

1. Mangin, B., Chpoun, A., Jacquin, L.: Experimental and numerical study of the fluidic thrust vectoring of a two-dimensional supersonic nozzle. AIAA Paper 2006-3666 (2006)

2. Wing, D.J., Giuliano, V.J.: Fluidic thrust vectoring of an axisymmetric exhaust nozzle at static conditions. ASME Fluids Engineering Division Summer Meeting, Paper FEDSM97-3228 (1997)

3. Bec, R., Bernard-Lepine, C., de Groote, K., Amouroux, F.: PERSEUS. A Nanosatellite Launch System Project Focusing on Innovation and Education. 2nd European Conference for Aerospace Sciences(EUCASS), Brussels (2007)

4. Wing, D.J.: Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle. NASA Technical Memorandum TM4574, Hampton Virginia (1994)

5. Flamm, J.D., Deere, K.A., Mason, M.L., Berrier, B.L., Johnson, S.K.: Experimental study of an axisymmetric dual throat fluidic thrust vectoring nozzle for supersonic aircraft application. AIAA Paper 2007-5084 (2007)

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