Experimental and numerical investigations on the ignition of rbcc gas-oxygen/kerosene rocket ejector

HIGHLIGHTS

  • who: RBCC Gas-Oxygen/Kerosene Rocket Ejector et al. from the School of Astronautics, Beihang University, Beijing, China have published the research work: Experimental and Numerical Investigations on the Ignition of RBCC Gas-Oxygen/Kerosene Rocket Ejector, in the Journal: International Journal of Aerospace Engineering of 13/07/2021
  • what: In this paper a thrust chamber with coaxial swirl injector for the ejection was developed and tested. oxygen (GOX) and kerosene acted as propellants. Since the model was characterized by circumferential symmetry, one-sixth of the combustion chamber was used for the simulation to simplify . . .

     

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