For the calculation of the combined cooling systems of propulsion engines

Adjoint heat transfer processes computational techniques for combined cooling systems of engines combustion chambers is proposed. The computational procedure of gas film, which permits to carry adjoint computation of gas film and cooling system elements at all chamber cross section including inner wall by unified scheme, has been present. The numerical calculations and verification results has been executed.

Keywords

propulsion engines, gas film, chambers, combined cooling, adjoint of a heat transfer

Publication date

10.01.2019

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GOST	Borisov D., Shuraev Y., Mironov V. For the calculation of the combined cooling systems of propulsion engines // Izvestiia Rossiiskoi akademii nauk. Energetika – 2018. – Issue 5 C. 101-108 [Electronic resource]. URL: http://ras.jes.su/energetika/s000233100003217-2-1-en (circulation date: 25.04.2024). DOI: 10.31857/S000233100003217-2
MLA	Borisov, D., Shuraev, Y., Mironov, V. "For the calculation of the combined cooling systems of propulsion engines." Izvestiia Rossiiskoi akademii nauk. Energetika 5 (2018):101-108. DOI: 10.31857/S000233100003217-2
APA	Borisov D., Shuraev Y., Mironov V. (2018). For the calculation of the combined cooling systems of propulsion engines. Izvestiia Rossiiskoi akademii nauk. Energetika (5), pp.101-108 DOI: 10.31857/S000233100003217-2

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