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Development of rotating supersonic combustion engine with swirling air-fuel injection

Ghazali, A. D. and Wahid, M. A. and Mazlan, M. A. and Saat, A. and Yasin, M. F. M. and Rahman, M. and Natrah, K. and Zain, Z. M. and Ardani, I. and Kasani, A. (2019) Development of rotating supersonic combustion engine with swirling air-fuel injection. In: 10th International Meeting of Advances in Thermofluids - Smart City: Advances in Thermofluid Technology in Tropical Urban Development, IMAT 2018, 16-17 Nov 2018, Grand Inna Hotel Kuta, Bali, Indonesia.


Official URL: http://www.dx.doi.org/10.1063/1.5086583


Rotating Supersonic Combustion Engine (RSCE) has the benefit of high-frequency operation, high thrust density for future generation engine. However, RSCE that is developed is still at infancy stage which requires further refined study especially in determining best mixing scheme. Therefore, the objective of this study is to develop and to test the new mixing scheme of RSCE using swirl injection system. The research also involves the investigation of the RSCE engine using supersonic combustion ignition system with various fuel-air injection configurations on the overall engine performance. This paper discussed about the engine and its ignition development using various configuration of swirl air-fuel injection system to achieve successful operation of rotating supersonic combustion engine.

Item Type:Conference or Workshop Item (Paper)
Uncontrolled Keywords:supersonic combustion, RSCE engine
Subjects:T Technology > TJ Mechanical engineering and machinery
Divisions:Mechanical Engineering
ID Code:89166
Deposited By: Narimah Nawil
Deposited On:26 Jan 2021 16:48
Last Modified:26 Jan 2021 16:48

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