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Experimental study on interference characteristics of hypersonic blunt body using opposing jet
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Binshu SHUI1, Feng XIE1, *, Hongyu WANG1, Gang WANG1, Yao JIA2, Tao LI2, Yanguang YANG3
Journal of Experiments in Fluid Mechanics | 2026, 40(2) : 1 - 12
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Journal of Experiments in Fluid Mechanics | 2026, 40(2): 1-12
• Special Topic on Research and Application Progress of Jet Flow in High-Speed Vehicles •
Experimental study on interference characteristics of hypersonic blunt body using opposing jet
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Binshu SHUI1, Feng XIE1, *, Hongyu WANG1, Gang WANG1, Yao JIA2, Tao LI2, Yanguang YANG3
Affiliations
  • 1Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
  • 2National Key Laboratory of Aerospace Physics in Fluids, Mianyang 621000, China
  • 3China Aerodynamics Research and Development Center, Mianyang 621000, China
Published: 2026-04-25 doi: 10.11729/syltlx20250035
Outline
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Opposing jet flow control technology has a broad application prospect and can achieve effective drag reduction control under the long penetration mode (LPM). In order to further study the opposing jet mode transition mechanism and the influence of freestream conditions on drag reduction control of hypersonic vehicles, wind tunnel tests were conducted on the blunt body model under different freestream total pressures (0.1 and 0.4 MPa), Mach numbers (Ma = 5, 6) and jet total pressure ratios. The structure of the spatial flow field and the surface pressure distribution of the model were obtained by using high-speed Schlieren and electronic pressure scanning valve. The results show that the LPM is extremely unstable, with strong unsteadiness and asymmetry, and the flow field presents axial and radial oscillations. At the transition phase, the flow field oscillates axially and changes continuously between LPM and short penetration mode (SPM). The SPM is stable and the flow field structure is axisymmetric. As the total pressure ratio increases, the surface pressure distribution of the model corresponds to the phase of jet mode transition. The critical total pressure ratio of the jet is affected by the freestream total pressure and Mach number. As the freestream total pressure increases, the critical total pressure ratio increases, and the total pressure ratio interval corresponding to LPM becomes larger. With the increase of incoming Mach number, the minimum total pressure ratio and critical total pressure ratio of sonic jet decreases, and the total pressure ratio interval corresponding to LPM becomes smaller.

opposing jet  /  flow control  /  hypersonic  /  drag reduction  /  penetration mode
税彬书, 谢峰, 王宏宇, 王刚, 贾尧, 李涛, 杨彦广. 高超声速来流下钝头体逆向射流干扰特性试验研究. 实验流体力学, 2026 , 40 (2) : 1 -12 . DOI: 10.11729/syltlx20250035
Binshu SHUI, Feng XIE, Hongyu WANG, Gang WANG, Yao JIA, Tao LI, Yanguang YANG. Experimental study on interference characteristics of hypersonic blunt body using opposing jet[J]. Journal of Experiments in Fluid Mechanics, 2026 , 40 (2) : 1 -12 . DOI: 10.11729/syltlx20250035
Year 2026 volume 40 Issue 2
112
40
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Article Info
doi: 10.11729/syltlx20250035
  • Receive Date:2025-04-24
  • Online Date:2026-10-22
  • Published:2026-04-25
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History
  • Received:2025-04-24
  • Revised:2025-06-03
  • Accepted:2025-06-11
Affiliations
    1Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
    2National Key Laboratory of Aerospace Physics in Fluids, Mianyang 621000, China
    3China Aerodynamics Research and Development Center, Mianyang 621000, China
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)
属
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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