Numerical Simulation of Scram-Jet Combustor Using Double Wall Injector

Abstract

development of efficient supersonic combustion scramjets is challenging with such a high speed flight within the atmosphere. The main focus of this study is to understand the fuel injection, fuel–air mixing, combustion in the high velocity and high enthalpy flow environment. A detailed cfd study was carried out to simulate the high speed reacting flows inside the combustion chamber. This paper presents the results of double wall injector having 0.295 mm diameter. The results obtained are very attractive and forced to think about the replacement of available fuel injector and enhanced the research to get more other way of fuel injection system so that the drawback of available fuel injector is completely eliminated. Using a double wall injector we get rapid air-fuel mixing with reduced pressure losses.

Authors and Affiliations

Dharmendra Kumar, Dr. Keshavendra Choudhary

Keywords

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  • EP ID EP24279
  • DOI -
  • Views 276
  • Downloads 9

How To Cite

Dharmendra Kumar, Dr. Keshavendra Choudhary (2017). Numerical Simulation of Scram-Jet Combustor Using Double Wall Injector. International Journal for Research in Applied Science and Engineering Technology (IJRASET), 5(5), -. https://europub.co.uk/articles/-A-24279