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

• Published in: Propulsion and Power Research
• Main Authors: Chouicha, Rachid, Sellam, Mohammed, Bergheul, Saïd
• Format: Journal Article
• Language: English
• Published: Elsevier 01.07.2020
• Subjects: Engineering Sciences; Mechanics; Fluidic thrust vectoring; Secondary injection; High temperature; Nozzle; Shock wave; Reacting gas

During the last years, several thrust control systems of aerospace rocket engines have been developed. The fluidic thrust vectoring is one of them; it is simple in design and offers a substantial gain in weight and in performance. Numbers of studies that deal with this subject are conducted on cold...