C. K. Akhil, K. Balaji, Saurabh Baranwal, Fariha Ainan Sohany, Shakuntala Gupta, Sadia Binte Sorowar, Singh Anup Tejnarayan
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Numerical analysis of scramjet combustion chamber under varied strut configuration
The objective of this paper is to enhance the combustion efficiency of a scram jet engine by varying the design parameters. The two dimensional numerical analysis is carried out with four different strut model using the k epsilon method for this study with the Mach number of 2 to evaluate the combustions efficiency and pressure loss. The results shows that strut model design 4 is providing the maximum efficiency of 99% with the total pressure loss of 3.08043 × 105 Pa compare to other strut model. The novelty of the model is to vary the two parameter like strut configuration along with fuel injection locations to enhance the combustion efficiency with minimum increment of pressure loss at supersonic conditions. This proposed method can be used for scramjet and supersonic related applications.
期刊介绍：
Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering.
Potential topics include, but are not limited to:
Trans-space vehicle systems design and integration
Air vehicle systems
Space vehicle systems
Near-space vehicle systems
Aerospace robotics and unmanned system
Communication, navigation and surveillance
Aerodynamics and aircraft design
Dynamics and control
Aerospace propulsion
Avionics system
Opto-electronic system
Air traffic management
Earth observation
Deep space exploration
Bionic micro-aircraft/spacecraft
Intelligent sensing and Information fusion
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