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Numerical Investigation on the Drags Trait of a Supersonic Inlet Curved Duct Near the Exit
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Yufen WEN, Jingjing GAO, Zheng ZHANG
Missiles and Space Vehicles | 2024, 47(1) : 24 - 29
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Missiles and Space Vehicles | 2024, 47(1): 24-29
Launch Vehicle and Missile
Numerical Investigation on the Drags Trait of a Supersonic Inlet Curved Duct Near the Exit
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Yufen WEN, Jingjing GAO, Zheng ZHANG
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  • China Academy of Launch Vehicle Technology,Beijing,100076
Published: 2024-02-25 doi: 10.7654/j.issn.2097-1974.20240105
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The matching design of thrust and drag is the core issue in the design of air-breathing vehicles. In order to obtain the drag trait of the inlet and reduce the interior drag, and then improve the overall performance of the air-breathing vehicles, a study on the cold-flow drag trait of a supersonic, twin-duct inlet is conducted with a CFD method. By comparing the flow characteristics and drag trait of the inlets with different length, turning angle, divergence ratio of the curved ducts, drag allocation proportion of different parts of the inlet is acquired and effects of the geometric parameters on the flow structure and drag are attained. Results indicate that a flow separation will probably generate in the curved duct of a twin-duct inlet at a cold-flow condition, which results in a large loss of the flow. It is noted that the drag of the curved duct accounts for majority of the entire inlet when there is no spilled flow. The drag of the curved duct can be reduced by decreasing the turning angle or increasing the divergence ratio of the curved duct. However, due to the interrelationship between the curved ducts' length and turning radius, the drag of the curved duct firstly reduces and then turns to rising with the increment of the curved ducts' length at a fixed design condition.

supersonic inlet  /  drag  /  curved duct  /  loss of the flow  /  separation
Yufen WEN, Jingjing GAO, Zheng ZHANG. Numerical Investigation on the Drags Trait of a Supersonic Inlet Curved Duct Near the Exit[J]. Missiles and Space Vehicles, 2024 , 47 (1) : 24 -29 . DOI: 10.7654/j.issn.2097-1974.20240105
Year 2024 volume 47 Issue 1
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doi: 10.7654/j.issn.2097-1974.20240105
  • Receive Date:2021-07-10
  • Online Date:2025-07-04
  • Published:2024-02-25
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  • Received:2021-07-10
  • Revised:2022-02-26
Affiliations
    China Academy of Launch Vehicle Technology,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
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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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