Cooling and friction reduction performance and mechanism of supersonic film cooling using hydrogen and hydrocarbon

WEI Jianfei; MI Zhenhao; ZHANG Silong; ZUO Jingying; LI Xin; QIN Jiang; BAO Wen

doi:10.11729/syltlx20230114

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WEI J F, MI Z H, ZHANG S L, et al. Cooling and friction reduction performance and mechanism of supersonic film cooling using hydrogen and hydrocarbon[J]. Journal of Experiments in Fluid Mechanics, doi: 10.11729/syltlx20230114

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Cooling and friction reduction performance and mechanism of supersonic film cooling using hydrogen and hydrocarbon

doi: 10.11729/syltlx20230114

1.
School of Energy Science and Engineering, Harbin Institute of Technology, Harbin　150001, China
2.
The 41st Institute of Fourth Academy of China Aerospace Science and Technology Corporation, Xi'an　710025, China

Received Date: 2023-09-06
Accepted Date: 2023-10-07
Rev Recd Date: 2023-09-23

Available Online: 2023-11-01

Abstract

Abstract

The essential difference of the turbulent state in the mixing layer contributes to the totally different behavior of the cooling and wall friction reduction performances of the hydrogen and hydrocarbon fuel films. The turbulent transport processes between the hydrogen film and the mainstream are much weaker than that of the hydrocarbon film making inert hydrogen to be rather superior in cooling and friction reduction applications. However, the film cooling performance severely deteriorates when the hydrogen film burns due to the severe heat release sources presented near the wall. On the other hand, the boundary layer combustion of hydrocarbon film can remarkably improve its original barely satisfactory cooling and friction reduction performance to be comparable to that of the hydrogen film due to the suppression of turbulent transport processes in the mixing layer and presence of heat absorption sources near the wall.
- supersonic film cooling,
- hydrogen,
- hydrocarbon,
- turbulent transport processes,
- large eddy simulation

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References(36)

References

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