Effect of Divergence Angles on the Performance of a Cavity-Based Scramjet Combustor
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6470-1_10
Reference20 articles.
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2. Shen W, Huang Y, Liu Z, You Y (2021) Mixing and transient combustion processes of scramjet combustor with transverse injector and hypermixer. Case Studies Thermal Eng 26:101104
3. Gruber MR, Baurle RA, Mathur T, Hsu KY (2001) Fundamental studies of cavity-based flameholder concepts for supersonic combustors. J Propul Power 17(1):146–153
4. Lu W, Zhansen Q, Liangjie G (2015) Numerical study of the combustion field in dual-cavity scramjet combustor. Procedia Eng 99:313–319
5. Ali M, Ahmed K, Kumar R, Alvi F (2011) Flowfield characteristics of oblique shocks generated using microjet arrays. In: 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, p 485
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