Numerical study for the flame deflector design of four-engine liquid rockets

References

• Akamine, M., Okamoto, K., Gee, K.L., Neilsen, T.B., Teramoto, S., Okunuki, T., & Tsutsumi, S. (2018). Effect of nozzle-plate distance on acoustic phenomena from supersonic impinging jet. AIAA Journal, 56(5), 1943–1952. https://doi.org/10.2514/1.J056504
   Web of Science ®Google Scholar
• Ali, P., Juhany, K., & Khalid, M. (2018). Numerical prediction of shock/boundary-layer interactions at high Mach numbers using a modified spalart-allmaras model. Engineering Applications of Computational Fluid Mechanics, 12(1), 459–472. https://doi.org/10.1080/19942060.2018.1451389
   Web of Science ®Google Scholar
• Alvi, F., & Iyer, K. (1999, May). Mean and unsteady flowfield properties of supersonic impinging jets with lift plates. Proceedings of the 5th AIAA/CEAS Aeroacoustics Conference, Bellevue, WA, USA. doi:10.2514/6.1999-1829.
   Google Scholar
• Basu, S., Saha, S., & Chakraborty, D. (2017). Numerical simulation of missile jet deflector. Journal of Spacecraft and Rockets, 54(4), 930–935. https://doi.org/10.2514/1.a33761
   Web of Science ®Google Scholar
• Brehm, C., Sozer, E., Moini-Yekta, S., Housman, J.A., Kiris, C., Barad, M.F., & Christopher, P. (2013, June). Computational prediction of pressure environment in the flame trench with launch vehicles. Proceedings of the 31st AIAA Applied Aerodynamics Conference, San Diego, CA, USA. doi:10.2514/6.2013-2538.
   Google Scholar
• Calhoon, W. (1998, July). Evaluation of afterburning cessation mechanisms in fuel rich rocket exhaust plumes. Proceedings of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, OH, USA. doi:10.2514/ 6.1998-3618.
   Google Scholar
• Daniel, C.A., & Vineet, A. (2007, July). Computational plume modeling of conceptual ARES vehicle stage tests. Proceedings of the 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cininnati, OH, USA. doi:10.2514/6.2007-5708.
   Google Scholar
• El-Amin, M., Sun, S., Heidemann, W., & Steinhagen, M. (2010). Analysis of a turbulent buoyant confined jet modeled using realizable k-ε model. Heat and Mass Transfer, 46(8-9), 943–960. https://doi.org/10.1007/s00231-010-0625-3
   Web of Science ®Google Scholar
• Fang, G., Wei, Z., Wu, Z., Du, R., & Wang, N. (2019). Experimental and numerical investigation of an embedded rocket ramjet combustor. Acta Astronautica, 165, 105–116. https://doi.org/10.1016/j.actaastro.2019.08.001
   Web of Science ®Google Scholar
• Ghalandari, M., Bornassi, S., Shamshirband, S., Mosavi, A., & Chau, K. (2019). Investigation of submerged structures’ flexibility on sloshing frequency using a boundary element method and finite element analysis. Engineering Applications of Computational Fluid Mechanics, 13(1), 519–528. https://doi.org/10.1080/19942060.2019.1619197
   Web of Science ®Google Scholar
• Hartfield, R., Jenkins, R., & Burkhalter, J. (2005, July). Optimizing a solid rocket motor boosted ramjet powered missile using a genetic algorithm. Proceedings of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Tucson, Arizona. doi:10.2514/6.2005-3507.
   Google Scholar
• Henderson, B. (2002). The connection between sound production and jet structure of the supersonic impinging jet. Journal of the Acoustical Society of America, 111(2), 735–747. https://doi.org/10.1121/1.1436069
   PubMed Web of Science ®Google Scholar
• Ignatius, J.K., Sathiyavageeswaran, S., & Chakravarthy, S.R. (2015). Hot-flow simulation of aeroacoustics and suppression by water injection during rocket liftoff. AIAA Journal, 53(1), 235–245. https://doi.org/10.2514/1.J053078
   Web of Science ®Google Scholar
• Jiang, C., Han, T., Gao, Z., & Lee, C. (2019). A review of impinging jets during rocket launching. Progress in Aerospace Sciences, 109, Article 100574. https://doi.org/10.1016/j.paerosci.2019.05.007
   Web of Science ®Google Scholar
• Koch, A.D. (2019). Optimal staging of serially staged rockets with velocity losses and fairing separation. Aerospace Science and Technology, 88, 65–72. https://doi.org/10.1016/j.ast.2019.03.019
   Web of Science ®Google Scholar
• Moraes, P., & Morgenstren, A. (2001). Evaluation of the effectiveness of VLS launcher flame deflector. Computers & Fluids, 30(5), 523–532. https://doi.org/10.1016/S0045-7930(01)00003-2
   Web of Science ®Google Scholar
• Nakai, Y., Fujimatsu, N., & Fujii, K. (2006). Experimental study of underexpanded supersonic Jet impingement on an inclined flat plate. AIAA Journal, 44(11), 2691–2699. https://doi.org/10.2514/1.17514
   Web of Science ®Google Scholar
• Negishi, H., Yamanishi, N., Arita, M., Namura, E., & Ohkubo, S. (2007, July). Numerical analysis of plume heating environment for H-IIA launch vehicle during powered ascent. Proceedings of the 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, USA. doi:10.2514/6.2007-5505.
   Google Scholar
• Panda, J., Mosher, R.N., & Porter, B.J. (2014). Noise source identification during rocket engine test firings and a rocket launch. Journal of Spacecraft and Rockets, 51(6), 1761–1772. https://doi.org/10.2514/1.a32863
   Web of Science ®Google Scholar
• Phillips, J.D. (1980). Flame deflector design, standard for. KSC-STD-Z-0012B. Kennedy Space Center.
   Google Scholar
• Poubeau, A., Paoli, R., & Cariolle, D. (2016). Evaluation of afterburning chemistry in solid-rocket motor jets using an off-line model. Journal of Spacecraft and Rockets, 53(2), 380–388. https://doi.org/10.2514/1.A33311
   Web of Science ®Google Scholar
• Prasad, J.K., Mehta, C., & Sreekanth, A.K. (1994). Impingement of supersonic jets on an axisymmetric deflector. AIAA Journal, 32(7), 1535–1538. https://doi.org/10.2514/3.12225
   Web of Science ®Google Scholar
• Rao, R., Sinha, K., Candler, G., Wright, M., & Levin, D. (1999, June). Numerical simulations of Atlas II rocket motor plumes. Proceedings of the 35th Joint Propulsion Conference and Exhibit, Los Angeles, CA, USA. doi:10.2514/6.1999-2258.
   Google Scholar
• Sakurai, T., Yuasa, S., Ando, H., Kitagawa, K., & Shimada, T. (2017). Performance and regression rate characteristics of 5-kN swirling-oxidizer-flow-type hybrid rocket engine. Journal of Propulsion and Power, 33(4), 891–901. https://doi.org/10.2514/1.b36239
   Web of Science ®Google Scholar
• Salih, S., Suliman, M., Rasani, M., Ariffin, A., & Yaseen, Z. (2019). Thin and sharp edges bodies-fluid interaction simulation using cut-cell immersed boundary method. Engineering Applications of Computational Fluid Mechanics, 13(1), 860–877. https://doi.org/10.1080/19942060.2019.1652209
   Web of Science ®Google Scholar
• Taghavi, S.R., Dehnavi, M.A., & Ghafouri, A. (2018). Numerical analysis of reactive turbulent flow in the thrust chamber of RD-108 engine rocket. Defense Technology, 15(4), 565–575. https://doi.org/10.1016/ j.dt.2018.12.004 doi: 10.1016/j.dt.2018.12.004
   Web of Science ®Google Scholar
• Tatsukawa, T., Nonomura, T., Oyama, A., & Fujii, K. (2016). Multi-objective aeroacoustic design exploration of launch-pad flame deflector using large-eddy simulation. Journal of Spacecraft and Rockets, 53(4), 751–758. https://doi.org/10.2514/1.A33420
   Web of Science ®Google Scholar
• Tsutsumi, S., Sarae, W., Ueda, H., & Hattori, A. (2018). Effect of rocket engine layouts on jet flowfield inside a launch pad. Journal of Spacecraft and Rockets, 55(6), 1537–1544. https://doi.org/10.2514/1.A34178
   Web of Science ®Google Scholar
• Tsutsumi, S., Takaki, R., Nakanishi, Y., Okamoto, K., & Teromoto, S. (2014). Acoustic generation mechanism of a supersonic jet impinging on deflectors. Proceedings of the 52nd Aerospace Sciences Meeting, National Harbor, Maryland, USA. doi:10.2514/6.2014-0882.
   Google Scholar
• Vatsa, V.N., & Wedan, B.W. (1990). Development of a multigrid code for 3-D Navier-Stokes equations and its application to a grid-refinement study. Computers & Fluids, 18(4), 391–403. https://doi.org/10.2514/6.1989-1791 doi: 10.1016/0045-7930(90)90029-W
   Web of Science ®Google Scholar
• Wei, Q., & Liang, G. (2017). Coupled Lagrangian impingement spray model for doublet impinging injectors under liquid rocket engine operating conditions. Chinese Journal of Aeronautics, 30(4), 1391–1406. https://doi.org/10.1016/j.cja.2017.06.011
   Web of Science ®Google Scholar
• Wu, J., Cai, G., He, B., & Zhou, H. (2016). Experimental and numerical investigations of vacuum plume interaction for dual hydrogen/oxygen thrusters. Vacuum, 128, 166–177. https://doi.org/10.1016/j.vacuum.2016.03.020
   Web of Science ®Google Scholar
• Yao, Z., Yao, J., & Sun, W. (2019). Adaptive RISE control of hydraulic systems with multilayer neural networks. IEEE Transactions on Industrial Electronics, 66(11), 8638–8647. https://doi.org/10.1109/TIE.2018.2886773
   Web of Science ®Google Scholar
• Zhang, J., Qu, Z., Fu, R., & He, Y. (2015). Experimental study on the transient thermal characteristics of an integrated deflector under the periodic impingement of a supersonic flame jet. International Journal of Heat and Mass Transfer, 85, 811–823. https://doi.org/10.1016/j.ijheatmasstransfer.2015.02.031
   Web of Science ®Google Scholar
• Zhou, Z., Lu, C., Zhao, C., & Le, G. (2020). Numerical simulations of water spray on flame deflector during the four-engine rocket launching. Advances in Space Research, 65(4), 1296–1305. https://doi.org/10.1016/j.asr.2019.11.008
   Web of Science ®Google Scholar
• Zidane, A., Haoui, R., Sellam, M., & Bouyahiaoui, Z. (2019). Numerical study of a nonequilibrium H2-O2 rocket nozzle flow. International Journal of Hydrogen Energy, 44(8), 4361–4373. https://doi.org/10.1016/j.ijhydene.2018.12.149
   Web of Science ®Google Scholar