Abstract
The multi-species numerical method has a strong demand in the simulation of propulsion systems, jet/flow control, and wind tunnel verification, due to it could simulate the change of species distribution caused by species transport, the flow field of thermally perfect gas. Based on NNW-FlowStar software, the multi-species numerical simulation ability was investigated and realized by the theoretical investigation and method verification in this paper, which will be applied in the thermally perfect gas CFD simulations of airplane, rocket, and hypersonic aircraft. Then, three examples were implemented to verify the multi-species numerical method investigated, and a conclusion was derived from the results. Firstly, the aerodynamic force coefficients achieved by the multi-species method realized in this paper are consistent with the ideal gas and experiment while the ideal gas is replaced by multi-species. Secondly, the accuracy and reliability of the multi-species numerical method realized in this paper were verified by comparing the results of three-dimensional hydrogen transverse injection and nitrogen opposing injection cases to the experimental one. Finally, the transverse jet of a typical general missile model (cone-cylinder-flare) was analyzed by the multi-species method, and the conclusion drawn from the results addresses that the multi-species numerical method investigated in this paper has the ability of a detailed analysis of the multi-species flowfield and application in industrial multi-species CFD simulation.
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References
Hou, L., Wang, D.: Comparison of shock/boundary interaction control with different types of jets. Physics of Gases 7(3), 38–44 (2022). (In Chinese)
Zhao, H., Gong, A., Liu, Z., et al.: Numerical study of lateral jet interaction at high altitude. Acta Aerodynamica Sinica 38(5), 996–1003 (2020). In Chinese
Fu, Y., Liu, Q., Ding, M., et. al: Analysis of gas model’s influence on aerodynamic characteristics for hypersonic vehicle over hot jet interaction flow field. Chinese Journal of Theoretical and Applied Mechanics 54(5), 1229–1241 (2022). In Chinese
Stahl, B., Emunds, H., Gülhan, A.: Experimental investigation of hot and cold side jet interaction with a supersonic cross-flow. Aerosp. Sci. Technol. 13, 488–496 (2009)
Stahl, B., Siebe, F., Gülhan, A.: Hot-gas side jet in a supersonic freestream. J. Spacecraft Rocket 47(6), 957–965 (2010)
Li, S., Wang, Z., Barakos, G., et al.: Research on the drag reduction performance induced by the counterflowing jet for waverider with variable blunt radii. Acta Astronautica 127, 120–130 (2016)
Sun, X., Guo, Z., Huang, W., et al.: Drag and heat reduction mechanism induced by a combinational novel cavity and counterflowing jet concept in hypersonic flows. Acta Astronautica 126, 109–119 (2016)
Deng, F., Xie, F., Qin, N., et al.: Drag reduction investigation for hypersonic lifting-body vehicles with aerospike and long penetration mode counterflowing jet. Aerospace Sci. Technol. 76, 361–373 (2018)
Wang, Z., Sun, X., Huang, W., et al.: Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows: a survey. Acta Astronautica 129, 95–110 (2016)
Qin, Q., Xu, J.: Aeroheating reduction for blunt body using aerodome jet. Acta Astronaut. 159, 17–26 (2019)
Dong, H., Zhang, X., Liu, S., et al.: Numerical and experimental study on opposing jet in hypersonic flow. Acta Aerodynamica Sinica 40(4), 101–109 (2022). (In Chinese)
Hayashi, K., Aso, S., Tani, Y.: Numerical study of thermal protection system by opposing jet. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA, Reno, Nevada, USA, (2005)
Liang, W., Zhang, X., Zhao, W., et al.: Research on the interference of side jet plume to a slender body in a subsonic or transonic freestream condition at large angle of attack. Air Space Defense 5(3), 38–43 (2022). (In Chinese)
Zhu, X., Li, F., Ou, D., et al.: Numerical simulation of flow control in lift-increase effect using air-blowing. Acta Aerodynamica Sinica 38(1), 66–72 (2020). (In Chinese)
Xue, F., Ren, Y., Xu, C., et al.: Aerodynamic characteristics of store during lateral jet assisted separation from cavity using free drop technique. Chinese J. Aeronaut. 36(1), 139–151 (2023)
Kumar, N., Bansal, A.: Flow and radiation modeling over a Martian entry vehicle. Acta Astronaut. 205, 172–184 (2023)
Meritt, R., Schetz, J., Marineau, E., et al.: Direct skin friction measurements at Mach 10 in a hypervelocity wind tunnel. J. Spacecraft Rocket 54(4), 871–881 (2017)
Mudford, N., O’Byrne, S., Neely, A., et. al: Hypersonic wind-tunnel free-flying experiments with onboard instrumentation. Journal of Spacecraft and Rocket 52(1), 231–241 (2015)
Chen, J., Wu, X., Zhang, J., et al.: FlowStar: general unstructured-grid CFD software for National Numerical Windtunnel (NNW) project. Acta Aeronautica et Astronautica Sinica 42(9), 625739 (2021)
Zhang, J., Zhou, N., Li, M., et. al: R & D and design of industrial CFD software for aeronautics and astronautics. J. Softw. 33(5), 1529–1550 (2022). In Chinese
Anderson, J.: Hypersonic and High-Temperature Gas Dynamics, 2nd edn. AIAA, Reston, Virginia (2006)
Yan, C., Fan, W.: Combustion, 3rd edn. Northwestern Polytechnical University Press, Xi’an (2016). In Chinese
Zheng, Y., Zou, J.: Numerical simulations of combustion processes in aerospace propulsion systems. Zhejiang University Press, Hangzhou (2018). In Chinese. f
Mayeur, J., Dumont, A., Destarac, D., et al.: Reynolds-Averaged Navier-Stokes Simulations on NACA0012 and ONERA-M6 Wing with the ONERA elsA Solver. AIAA J. 54(9), 2671–2687 (2016)
Rogers, R.: A Study of the Mixing of Hydrogen Injected Normal to a Supersonic Airstream. NASA, Hampton, VA (1971)
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The authors would like to acknowledge the support of the Academician Workstation of Aerospace Flight Frontier Technology for this work.
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Cheng, F., Fu, Y., Zhang, Y., Zhang, J., Zhou, N., Zhao, H. (2024). Investigation and Applications of Multi-species Numerical Method Based on NNW-FlowStar. In: Qu, Y., Gu, M., Niu, Y., Fu, W. (eds) Proceedings of 3rd 2023 International Conference on Autonomous Unmanned Systems (3rd ICAUS 2023). ICAUS 2023. Lecture Notes in Electrical Engineering, vol 1170. Springer, Singapore. https://doi.org/10.1007/978-981-97-1107-9_14
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DOI: https://doi.org/10.1007/978-981-97-1107-9_14
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