Vortex Combustion Chamber with Angular Flame Stabilizer: Design and Experimental Investigations
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-3788-0_3
Reference17 articles.
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3. Heath C (2016) Parametric modeling investigation of a radially-staged low-emission aviation combustor. In: 54th AIAA aerospace sciences meeting, p 1394
4. Magerramova LA, Nozhnitsky YA, Volkov SA, Volkov ME, Chepurnov VZ, Belov SV, Verbanov IS, Zaikin SV (2019) Prospects of application of additive technologies to develop parts and components of gas turbine engines and ramjets. Vestnik Samara Univ Aerosp Mech Eng 18(3):81–98. https://doi.org/10.18287/2541-7533-2019-18-3-81-98
5. Aleksandrov YB, Vafin II, Volkov SA, Mingazov BG (2018) Investigating the formation of temperature patterns in gas turbine engine combustion chambers. Eng J Sci Innov 1(73). https://doi.org/10.18698/2308-6033-2018-1-1716
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