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Experimental and Numerical Study on Phase Change Transpiration Cooling for a Wedge-shaped Nose Cone with a Gradient Porosity Layout
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Yifei LIU1, Luguang LIU2, Yibin DOU2, Taolue LIU1, Fei HE1
Missiles and Space Vehicles | 2024, 47(5) : 81 - 91
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Missiles and Space Vehicles | 2024, 47(5): 81-91
Environment and Test
Experimental and Numerical Study on Phase Change Transpiration Cooling for a Wedge-shaped Nose Cone with a Gradient Porosity Layout
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Yifei LIU1, Luguang LIU2, Yibin DOU2, Taolue LIU1, Fei HE1
Affiliations
  • 1 University of Science and Technology of China,Hefei,230026
  • 2 Shanghai Electro-mechanical Engineering Institute,Shanghai,201109
Published: 2024-10-25 doi: 10.7654/j.issn.2097-1974.20240512
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In order to improve the transpiration cooling efficiency at the stagnation point of the nose cone of the near space vehicle, a wedge-shaped porous nose cone with a gradient porosity layout is proposed and the phase change transpiration cooling is experimentally and numerically investigated under different coolant injection ratio. The experimental results indicate that the gradient porosity layout can effectively improve the cooling efficiency at the stagnation point and the overall temperature uniformity of the porous surface. When the coolant injection ratio $M$ is 0.125%, the cooling efficiency at the stagnation point is increased by 52.4%, and the overall cooling efficiency is increased by 31.7%. The numerical results indicate that the gradient porosity layout increases the coolant mass flux at the leading edge and optimizes coolant distribution by moving the maximum pressure value at the stagnation point downstream. When the coolant injection ratio $M ={0.15}\%$, the coolant mass flux at the stagnation point is increased 76%. In addition, the film formed by the coolant flows out of the porous structure is more uniform.

active thermal protection  /  transpiration cooling  /  porous media  /  liquid-gas phase change  /  thermal protection
Yifei LIU, Luguang LIU, Yibin DOU, Taolue LIU, Fei HE. Experimental and Numerical Study on Phase Change Transpiration Cooling for a Wedge-shaped Nose Cone with a Gradient Porosity Layout[J]. Missiles and Space Vehicles, 2024 , 47 (5) : 81 -91 . DOI: 10.7654/j.issn.2097-1974.20240512
Year 2024 volume 47 Issue 5
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doi: 10.7654/j.issn.2097-1974.20240512
  • Receive Date:2024-02-22
  • Online Date:2025-07-04
  • Published:2024-10-25
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  • Received:2024-02-22
  • Revised:2024-04-24
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    1 University of Science and Technology of China,Hefei,230026
    2 Shanghai Electro-mechanical Engineering Institute,Shanghai,201109
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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