[1] Trenton Z.Y., Design and testing of an unmanned aerial to underwater vehicle. 14th AIAA Aviation Technology, Integration, and Operations Conference, Atlanta, USA, 2014, 2: 1–15.
[2] He Z.X., Zheng Z.S., Ma D.L., et al., Development of foreign trans-media aircraft and its enlightenment to China. Ship Science and Technology, 2016, 38(09): 152–157.
[3] Lv K., Liu Y., You C., et al., Hydrodynamic investigations of a cross-domain vehicle with the capability of high-speed cruising on water surface. Ocean Engineering, 2023, 280: 114688.
[4] Liu J.Y., Yu Y., Experimental scheme design of constrained vehicle in a trans-media process and CFD analysis of scheme. Acta Aeronautica et Astronautica Sinica, 2023, 44(21): 528488.
[5] Rober S., Mirko K., Fast aquatic escape with a jet thruster. IEEE/ASME Transactions on Mechatronics, 2017, 22(01): 217–226.
[6] Li P.F., Huang L.Y., Xia Z.X., et al., Study on working characteristics boron-based fuel rich propellant trans-media ramjet. Journal of Solid Rocket Technology, 2022, 45(5): 662–667.
[7] Shan R.L., Research on hybrid aerial-aquatic propeller optimization and experiment. Shanghai Jiaotong University, Shanghai, China, 2021.
[8] Qi D., Feng J.F, Li Y.L., Anti-ship weapons with water-air medium spanning capability. Aerodynamic Missile Journal, 2015, 12: 50–53.
[9] Bossard J., Thomas M., Customized turbomachinery for solid-propellant air turbo rockets. 33rd Joint Propulsion Conference & Exhibit, Huntsville, USA, 1997.
DOI: 10.2514/6.1997-3257.
[10] Thomas M., Monorotor turbomachinery for air-turbo- rocket propulsion. 31st Joint Propulsion Conference and Exhibit, Huntsville, USA, 1995, Paper No: AIAA 95-2804.
[11] Kiely D.H., Moore J.T., Hydrocarbon fueled UUV power systems. IEEE, Proceedings of the 2002 Workshop on Autonomous Underwater Vehicles, 2002.
DOI: 10.1109/AUV.2002.1177214.
[12] Qin K, Wang H.W., Qi J., et al., Aerodynamic design and experimental validation of high-pressure ratio partial admission axial impulse turbines for unmanned underwater vehicles. Energy, 2022, 239: 122242.
[13] Kacker S.C., Okapuu U., A mean line prediction method for axial flow turbine efficiency. Journal of Engineering for Power, 1982, 104: 111–119.
[14] Reza A.T., Tousi A.M., Flow pattern improvement in nozzle-rotor axial gap in impulse turbine. Aircraft Engineering and Aerospace Technology, 2014, 86(2): 108–116.
[15] Reza A.T., Tousi A.M., Experimental and numerical investigation of design optimization of a partial admitted supersonic turbine. Propulsion and Power Research, 2013, 2(1): 70–83.
[16] Reza A.T., Tousi A.M., Effects of nozzle arrangement angle on the performance of partially admitted turbines. Journal of Mechanical Science and Technology, 2018, 32(1): 455–464.
[17] Reza A.T., Tousi A.M., An empirical model for partially admitted turbine efficiency. Aircraft Engineering & Aerospace Technology, 2015, 87(3): 238–248.
[18] Smirnov M., Sebelev A., Zabelin N., et al., Effects of hub endwall geometry and rotor leading edge shape on performance of supersonic axial impulse Part I. Proceedings of 12th European Conference on Turbomachinery Fluid dynamics & Thermodynamics. European Turbomachinery Society, Stockholm, Sweden, 2017, Paper ID: ETC2017-100.
[19] Jeong E., Park P.G., Sang H.K., et al., Effect of nozzle-rotor clearance on turbine performance. ASME 2006 2nd Joint U.S.-European Fluids Engineering Summer Meeting Collocated With the 14th International Conference on Nuclear Engineering, Miami, USA, 2006, 2: 1–6.
[20] Piotr K., Łukasz W., Tomasz S., et al., Selection of optimum degree of partial admission in a laboratory organic vapour microturbine. Energy Conversion and Management, 2019, 202: 112189.
[21] Cho S.Y., Cho C.H., Kim C., Performance prediction on a partially admitted small axial-type turbine. JSME International Journal, 2007, 49(4): 1290–1297.
[22] Shao D., Analysis to the power system of the trans-media vehicle. Aerospace Power, 2020, 1: 12–15.
[23] Jiang B., Luo K., Gao A.J., et al., A design approach of micro partial admission impulse turbine. Torpedo Technology, 2015, 23(5): 353–358.
[24] Jiang B., Luo K., Gao A.J., et al., New design approach of scarfed nozzle in underwater impulse turbine. Torpedo Technology, 2015, 23(4): 296–300.
[25] Zhao Y.S., Underwater turbine principle. Northwestern Polytechnical University Press, Xi’an, China, 2002.
[26] Chiong M.S., Rajoo S., Romagnoli A., et al., Integration of meanline and one-dimensional methods for prediction of pulsating performance of a turbocharger turbine. Energy Conversion & Management, 2014, 81(5): 270–281.
[27] Menter F.R., Two-equation eddy-viscosity turbulence models for engineering applications. AIAA Journal, 1994, 32(8): 1598–1605.
[28] Obert B., Cinnella P., Comparison of steady and unsteady RANS CFD simulation of a supersonic ORC turbine. Energy Procedia, 2017, 129: 1063–1070.
[29] Seume J.R., Peters M., Kunte H., Design and test of a 10 kW ORC supersonic turbine generator. Journal of Physics: Conference Series. Varenna, Italy, 2017, 821(1): 012023.
[30] Zhang R.G., Aerodynamic performance research on ultra-high expansion ratio turbine, Harbin Institute of Technology, Harbin, China, 2014.
[31] Waesker M., Buelten B., Kienzle N., et al., Optimization of supersonic axial turbine blades based on surrogate models. ASME Turbo Expo: Turbomachinery Technical Conference and Exposition, Cincinnati, Ohio, USA, 2020, Paper No: GT2020-14465.
[32] Colclough C.D., Design of turbine blades suitable for supersonic relative inlet velocities and the investigation of their performance in cascades: Part II-Experiments, results and discussion. Journal of Mechanical Engineering Science, 1966, 8(2): 185–197.
[33] Qin K., Wang H., Qi J., et al., Aerodynamic design and experimental validation of high pressure ratio partial admission axial impulse turbines for unmanned underwater vehicles. Energy, 2022, 239: 122242.
[34] Qin K., Wang H., Wang X., et al., Thermodynamic and experimental investigation of a metal fuelled steam Rankine cycle for Unmanned Underwater Vehicles. Energy Conversion and Management, 2023, 223: 113281.
[35] Peng N., Wang E., Wang W., Design and analysis of a 1.5 kW single-stage partial-admission impulse turbine for low-grade energy utilization. Energy, 2023, 268: 126631.
[36] Zengin İ., Erdoğan B., Benim A.C., CFD and Taguchi based optimization of air driven single stage partial admission axial turbine blade profiles. Energy, 2024, 290: 130333.
[37] Tokuyama K., Funazaki K., Kato H., et al., A study of the unsteady flow field and turbine vibration characteristics of the supersonic partial admission turbine for a rocket engine. International Gas Turbine Congress, Tokyo, Japan, 2015, 15: 962–972.
[38] Cho S.Y., Cho C.H., Kim C., Performance prediction on a partially admitted small axial-type turbine. JSME International Journal Series B-fluids and Thermal Engineering, 2007, 49(4): 1290–1297.
[39] Verneau A., Supersonic turbines for organic fluid Rankine cycles from 3 to 1300 kW: Small high pressure ratio turbines. Von Karman Institute for Fluid Dynamics, 1987, 7: 15–18.
[40] Stenning A.H., Design of turbines for high-energy-fuel low-power-output applications. MIT Dynamic Analysis and Control Laboratory, Cambridge, MA, USA, 1953.
[41] Suter P., Traupel W., Untersuchungen über den ventilationsverlust von turbinenrädern. Verlag-Leemann, Berlin, 1959.
[42] Doyle M.D.C., Theories for predicting partial-admission losses in turbines. Journal of the Aerospace Sciences, 2014, 29(4): 489–490.
[43] Cho S.Y., Choi S.K., Performance characteristics of a micro air grinder operated by a two-stages axial-type turbine. JSME International Journal, 2006, 49(2): 443–449.
[44] Jiao J.F., Song H.C., et al., Research on the effect of inter-row spacing on the shock wave structure and performance of turbine. Journal of Engineering Thermophyics, 2017, 38(1): 61–67.
[45] Goeing M., Nozzle design optimization by method-of-characteristics. 26th Joint Propulsion Conference, Orlando, Florida, USA, 1990.
[46] Li R., Xu J., Yu K., et al., Design and analysis of the scramjet nozzle with contact discontinuity. Aerospace Science and Technology, 2021, 113: 106695.
[47] Zucrow M.J., Hoffman J.D., Gas dynamics. Volumes I, II, John Wiley & Sons, Inc, Canada, 1977.
[48] Xu J.L., Mo J.W., Yu Y., et al., Exhaust system of high speed vehicle engine. National Defense Industry Press, Beijing, 2019.