收藏切换
Characteristics of boundary layer stability of HyTRV model bottom
收藏切换
Shuyi LIU1, Ao WANG1, Maochang DUAN1, Yang XU2, Ganglei HUANG1, *, Jianqiang CHEN1
Journal of Experiments in Fluid Mechanics | 2026, 40(1) : 135 - 145
Less
收藏切换
Journal of Experiments in Fluid Mechanics | 2026, 40(1): 135-145
• Fundamental Research and Application •
Characteristics of boundary layer stability of HyTRV model bottom
Full
Shuyi LIU1, Ao WANG1, Maochang DUAN1, Yang XU2, Ganglei HUANG1, *, Jianqiang CHEN1
Affiliations
  • 1Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
  • 2Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
Published: 2026-02-25 doi: 10.11729/syltlx20240014
Outline
收藏切换

The HyTRV (Hypersonic Transition Research Vehicle) is designed for the study of hypersonic complex three-dimensional boundary layer transition, the shape of which is close to that of the real aircraft. The principal objective of this research is to gain deeper understanding of the stability characteristics and transition mechanism of the boundary layer over the HyTRV model and verify the results of numerical simulation and theoretical analysis. In the Mach 6 wind tunnel, the transition front and unstable wave evolution characteristics at the bottom of the HyTRV model, obtained by the infrared thermal imaging technology and high-frequency pressure sensors respectively, were compared with the results of one-dimensional stability analysis. At the angle of attack of 2 degrees, the instability crossflow region on the windward side, which is located after the front of transition at the centerline, shrinks and moves backwards compared to the results with zero angle of attack. Broadband high-frequency signals, containing multiple disturbances in different frequency bands, were found in the crossflow region. The interaction between various disturbances widens the frequency spectrum. Then the boundary layer appears to breakdown. The signal amplitude reaches saturation before the transition is complete.

lifting body  /  crossflow instability  /  hypersonic wind tunnel  /  boundary layer transition  /  eN method
刘姝怡, 王傲, 段茂昌, 徐洋, 黄刚雷, 陈坚强. HyTRV标模下表面边界层稳定性特征. 实验流体力学, 2026 , 40 (1) : 135 -145 . DOI: 10.11729/syltlx20240014
Shuyi LIU, Ao WANG, Maochang DUAN, Yang XU, Ganglei HUANG, Jianqiang CHEN. Characteristics of boundary layer stability of HyTRV model bottom[J]. Journal of Experiments in Fluid Mechanics, 2026 , 40 (1) : 135 -145 . DOI: 10.11729/syltlx20240014
Year 2026 volume 40 Issue 1
63
24
Cite this Article
BibTeX
Article Info
doi: 10.11729/syltlx20240014
  • Receive Date:2024-02-02
  • Online Date:2026-10-22
  • Published:2026-02-25
Article Data
Affiliations
History
  • Received:2024-02-02
  • Revised:2024-02-21
  • Accepted:2024-02-27
Affiliations
    1Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
    2Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
References
Share
https://castjournals.cast.org.cn/joweb/syltlx/EN/10.11729/syltlx20240014
Share to
QR

Scan QR to access full text

Cite this article
BibTeX
Citations
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
关闭全屏
  • BibTeX
  • EndNote
  • RefWorks
  • TxT