2021
DOI: 10.1007/978-3-030-69421-0_5
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Numerical Calculation of the Heat Sink Parameters of the Shell Turbine Vanes at the Modeling of the Heat-Protective Coating with a Different Number of Layers

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Cited by 8 publications
(7 citation statements)
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“…As a result, the structure is facilitated, metal is saved, the technology is simplified and the cost of structures is reduced. The results of the research confirm the possibility of using prestress taking into account the parameters for different cases in a cylindrical shell [ 22 , 23 , 24 , 25 , 26 , 27 , 28 , 29 , 30 , 31 , 32 , 33 , 34 , 35 , 36 , 37 , 38 , 39 , 40 , 41 , 42 , 43 , 44 , 45 , 46 , 47 , 48 , 49 ].…”
Section: Resultssupporting
confidence: 62%
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“…As a result, the structure is facilitated, metal is saved, the technology is simplified and the cost of structures is reduced. The results of the research confirm the possibility of using prestress taking into account the parameters for different cases in a cylindrical shell [ 22 , 23 , 24 , 25 , 26 , 27 , 28 , 29 , 30 , 31 , 32 , 33 , 34 , 35 , 36 , 37 , 38 , 39 , 40 , 41 , 42 , 43 , 44 , 45 , 46 , 47 , 48 , 49 ].…”
Section: Resultssupporting
confidence: 62%
“…In any case, the pitch, according to the recommendations of [ 22 , 23 , 24 , 25 , 26 , 27 , 28 , 29 , 30 , 31 , 32 , 33 , 34 , 35 , 36 , 37 , 38 , 39 , 40 ], should be less than the half-wave length— , and it should be selected according to the conditions of the tasks solved by prestressing and a technical and economic comparison of options.…”
Section: Resultsmentioning
confidence: 99%
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