Comparison of the different shapes of extruded annular nozzle on the fuel mixing of the hydrogen jet at supersonic combustion chamber
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DOI: 10.1016/j.energy.2023.128142
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- Amin Hassanvand & M. Barzegar Gerdroodbary & Amir Musa Abazari, 2021. "Injection of hydrogen sonic multi-jet on inclined surface at supersonic flow," International Journal of Modern Physics C (IJMPC), World Scientific Publishing Co. Pte. Ltd., vol. 32(03), pages 1-14, March.
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- Li, Zhixiong & Manh, Tran Dinh & Barzegar Gerdroodbary, Mostafa & Nam, Nguyen Dang & Moradi, R. & Babazadeh, Houman, 2020. "The effect of sinusoidal wall on hydrogen jet mixing rate considering supersonic flow," Energy, Elsevier, vol. 193(C).
- F. Pish & Tran Dinh Manh & M. Barzegar Gerdroodbary & Nguyen Dang Nam & Rasoul Moradi & Houman Babazadeh, 2020. "Computational study of the cavity flow over sharp nose cone in supersonic flow," International Journal of Modern Physics C (IJMPC), World Scientific Publishing Co. Pte. Ltd., vol. 31(06), pages 1-12, June.
- Peng, Yeping & Barzegar Gerdroodbary, M. & Sheikholeslami, M. & Shafee, Ahmad & Babazadeh, Houman & Moradi, R., 2020. "Mixing enhancement of the multi hydrogen fuel jets by the backward step," Energy, Elsevier, vol. 203(C).
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Cited by:
- Ben Ali, Naim & Basem, Ali & Ghodratallah, Pooya & Singh, Pradeep Kumar & jasim, Dheyaa J. & Sultan, Abbas J. & Eladeb, Aboulbaba & Kolsi, Lioua & El-Shafay, A.S., 2024. "The usage of non-aligned multi-circular winding injectors for efficient fuel mixing inside the scramjet engine," Energy, Elsevier, vol. 298(C).
- Wei, Dechen & Jiao, Yuanyuan & Zhang, Ning & Gao, Hongyang & Yu, Hao, 2024. "The role of annular 2-lobe nozzle in a strut injection system on the mechanism of fuel distribution at a scramjet engine," Energy, Elsevier, vol. 301(C).
- Huang, Dian, 2024. "Using extruded circular multi-injectors to improve fuel jet mixing and distribution in combustion chambers of scramjet," Energy, Elsevier, vol. 288(C).
- Wei, Dechen & Jiao, Yuanyuan & Zhang, Ning & Fan, Yukun, 2023. "Effect of shock generator on fuel mixing in an annular single lobe transverse nozzle at the supersonic combustion chamber of a scramjet engine using computational fluid dynamics," Energy, Elsevier, vol. 283(C).
- Dai, Zuocai & Zou, Yunhe & Chow, Limeng, 2024. "The role of the shock generator on the mixing performance of hydrogen jet released from the extruded transverse 3-lobe nozzle in a scramjet engine," Energy, Elsevier, vol. 288(C).
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Keywords
Combustion chamber; Supersonic flow; Fuel mixing; Scramjet engine; Numerical study; Spacecraft;All these keywords.
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