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Characteristics of Whole-vehicle Drag Reduction in High-speed Vehicle Through Opposing Jet Flow
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Tianpeng YANG, Junpeng HUI, Jiangpeng YU, Likun ZHANG
Missiles and Space Vehicles | 2024, 47(6) : 1 - 7
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Missiles and Space Vehicles | 2024, 47(6): 1-7
Launch Vehicle and Missile
Characteristics of Whole-vehicle Drag Reduction in High-speed Vehicle Through Opposing Jet Flow
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Tianpeng YANG, Junpeng HUI, Jiangpeng YU, Likun ZHANG
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  • Beijng Institute of Space Long Mach Vehicle,Beijing,100076
Published: 2024-12-25 doi: 10.7654/j.issn.2097-1974.20240601
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To study the drag reduction characteristics of head opposing jet flow for the whole high-speed vehicle, a calculation model is established for sphere bicone, and flow field is solved by using multi-component axial symmetry Navier-Stokes equations. The influence laws of the opposing jet on the wave drag, friction drag, and base drag are studied by using the height of free stream, and the total pressure ratio of the jet and free stream. The calculation results show that the increase of the total pressure ratio reduces the wave drag and base drag by changing the flow field structure, and it leads to a temperature decrease and velocity gradient increase within the boundary layer. The dominant boundary velocity gradient can lead to an increase in friction drag. For high-altitude conditions, the friction drag has a high proportion of total drag and a better drag reduction effect, so it is better to choose an appropriate total pressure ratio. For low-altitude conditions, the base drag has a high proportion of total drag and a better drag reduction effect, so it is better to choose a high total pressure ratio. Considering the cost-effectiveness ratio of drag reduction and opposing jet mass flow, high-altitude flight conditions with a small total pressure ratio can be chosen.

numerical simulation  /  opposing jet  /  drag reduction  /  height of free stream  /  total pressure ratio of the jet and free stream
Tianpeng YANG, Junpeng HUI, Jiangpeng YU, Likun ZHANG. Characteristics of Whole-vehicle Drag Reduction in High-speed Vehicle Through Opposing Jet Flow[J]. Missiles and Space Vehicles, 2024 , 47 (6) : 1 -7 . DOI: 10.7654/j.issn.2097-1974.20240601
Year 2024 volume 47 Issue 6
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doi: 10.7654/j.issn.2097-1974.20240601
  • Receive Date:2024-07-07
  • Online Date:2025-07-04
  • Published:2024-12-25
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  • Received:2024-07-07
  • Revised:2024-11-26
Affiliations
    Beijng Institute of Space Long Mach Vehicle,Beijing,100076
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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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