The Flow Control Technology for Hypersonic Flights
DOI:
https://doi.org/10.54097/t327a833Keywords:
hypersonic aircraft, flow control technology, case analysis, history.Abstract
The hypersonic aircraft has important implications for society. This technology helps military operations proceed more smoothly and easily. It also opens up new possibilities for scientific exploration, such as exploring space and meteorological observation. In this essay, the perspective of s specific system on the hypersonic aircraft, the flow control, is used to illustrate the feasibility of adapting to high-altitude aerodynamic phenomena, including turbulence, vortexes and boundary layers. The advantages and effectiveness of the flow control technology are shown clearly by introducing two cases. Through analyzing the design aerodynamic characteristics of the typical vehicle, X-51A, the passive flow control is demonstrated as a good way to improve flow stability and overall efficiency due to the streamlined shape and the wave rider design. The HAWC successfully utilizes the active and MHD flow control system. It adjusts the velocity of fluid flow by changing the direction and strength of the magnetic field. Thus, not only can the precise control be guaranteed, but also the fuel consumption is reduced. Despite current benefits, for future research, the scientist should focus more on the new materials and the combination and optimization of several flow control technologies.
Downloads
References
[1] Wang, J., Han, C., Huang, Y., Liu, J., & He, Y. (2024). A review of international hypersonic technology developments in 2023. Journal of Tactical Missile Technology, 01, 7-19. doi: 10.16358/j.issn.1009-1300.20240503.
[2] Yang, Y. Z., Yang, J. L., & Fang, D. N. (2008). Research progress on thermal protection materials and structures of hypersonic vehicles. Applied Mathematics and Mechanics, 29, 51-60.
[3] Guerrero, J., Sanguineti, M., & Wittkowski, K. (2018). CFD study of the impact of variable cant angle winglets on total drag reduction. Aerospace, 5(4), 126.
[4] Robinson, S. T. E. P. H. E. N. K. (1991). Coherent motions in the turbulent boundary layer. Annual review of fluid mechanics, 23(1), 601-639.
[5] Casper, K., Beresh, S., Henfling, J., Spillers, R., Pruett, B., & Schneider, S. (2009, June). Hypersonic wind-tunnel measurements of boundary-layer pressure fluctuations. In 39th AIAA fluid dynamics conference (p. 4054).
[6] Teng, Z., Zhou, Z., Zhang, Z., Xu, K., & Gao, Z. (2024). Numerical simulation study on MHD flow control at hypersonic speeds. Aerodynamic Research and Experimentation, 01, 86-99. doi: 10.20118/j.issn2097-258X.2024.01.007.
[7] Kuranov, A. L., & Sheikin, E. G. (2003). Magnetohydrodynamic Control on hypersonic Aircraft under" AJAX" concept. Journal of Spacecraft and Rockets, 40(2), 174-182.
[8] Yi, W., Wang, Y., Pang, L., Xiao, L., Ding, Z., & Duan, P. (2019). Progress in plasma/MHD flow control research of air intakes. Acta Mechanica Sinica, 51(2), 311-321.
Downloads
Published
Issue
Section
License
Copyright (c) 2025 Highlights in Science, Engineering and Technology
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.
