2019
DOI: 10.1016/j.ijheatmasstransfer.2019.118433
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Effect of gaseous coolant temperature on the transpiration cooling for porous wall in the supersonic flow

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Cited by 21 publications
(5 citation statements)
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“…Let us now consider the possible causes of the observed behavior of the flame in the considered coaxial burner. As it was shown recently in [22], the important roles in the heat transfer near the porous (or perforated) wall belong both to the dissipation of kinetic energy and convective heat transfer in the formed boundary layer. In view of this, the flow separation from the perforated wall due to the gas injection defines the specific mode of heat transfer to the wall.…”
Section: Resultsmentioning
confidence: 84%
See 1 more Smart Citation
“…Let us now consider the possible causes of the observed behavior of the flame in the considered coaxial burner. As it was shown recently in [22], the important roles in the heat transfer near the porous (or perforated) wall belong both to the dissipation of kinetic energy and convective heat transfer in the formed boundary layer. In view of this, the flow separation from the perforated wall due to the gas injection defines the specific mode of heat transfer to the wall.…”
Section: Resultsmentioning
confidence: 84%
“…However, at the same time, it is also possible to utilize gaseous heat screens. As is shown in [22], gas injection into the flow through the porous wall can affect the temperature of the wall noticeably. Therefore, such an approach is suitable for the maintenance of stable combustion in low-reactive combustible mixtures, including lean mixtures.…”
Section: Introductionmentioning
confidence: 93%
“…1,7 Even so it has been invented in the 1950s, 8 due to both advances made in manufacturing and the need for greater cooling efficiency, recently transpiration cooling has come back into the focus of research and has been intensively studied experimentally, analytically and numerically. 5,[9][10][11][12][13][14] The porous materials used for transpiration cooling have to meet certain requirements, like high porosity, light-weight, precise geometry, and additionally, for turbine blades, 6 great material strength. Commonly used types of porous materials are sintered metal or ceramic porous media 7 and ceramic matrix composites, 15 leaving the pores to be a result of randomness.…”
Section: Transpiration Coolingmentioning
confidence: 99%
“…Some applications nowadays considered for transpiration cooling include scramjet combustion chambers, 4 rocket thrust chambers, 5 turbine blades, 6 and others 1,7 . Even so it has been invented in the 1950s, 8 due to both advances made in manufacturing and the need for greater cooling efficiency, recently transpiration cooling has come back into the focus of research and has been intensively studied experimentally, analytically and numerically 5,9‐14 …”
Section: Introductionmentioning
confidence: 99%
“…Some applications nowadays considered for transpiration cooling include scramjet combustion chambers [4], rocket thrust chambers [5], turbine blades [6] and others [1,7]. Even so it has been invented in the 1950's [8], due to both advances made in manufacturing and the need for greater cooling efficiency, recently transpiration cooling has come back into the focus of research and has been intensively studied experimentally, analytically and numerically [5,9,10,11,12,13,14].…”
Section: Introductionmentioning
confidence: 99%