WITHDRAWN: Effect of reacting gas on the fluidic thrust vectoring of an axisymmetric nozzle-Reference-Cited by-同舟云学术

WITHDRAWN: Effect of reacting gas on the fluidic thrust vectoring of an axisymmetric nozzle

Published:2020-07 Issue: Volume: Page:
ISSN:2212-540X
Container-title:Propulsion and Power Research
language:en
Short-container-title:Propulsion and Power Research

Author:

Chouicha R.,Sellam M.,Bergheul S.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Fuel Technology,Aerospace Engineering,Automotive Engineering

Reference32 articles.

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3. Thrust vectoring control of supersonic flow through an orifice injector;Mnafeg;Int. J. Mech. Aero. Ind. Mech. Manuf. Eng,,2015

4. Experimental and computational investigation of multiple injection ports in a convergent-divergent nozzle for fluidic thrust vectoring, 21st AIAA Applied Aerodynamics Conference, Orlando, Florida;Waithe,2003

5. A system study on fluidic thrust vectoring, 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conferences;Van Pelt;Glasgow, Scotland,2015

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