Статті в журналах з теми "Hypersonic inlet design"
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Zhai, Jian, Chen-An Zhang, Fa-Min Wang, and Wei-Wei Zhang. "Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines." International Journal of Modern Physics B 34, no. 14n16 (June 4, 2020): 2040074. http://dx.doi.org/10.1142/s0217979220400743.
Повний текст джерелаSaheby, Eiman B., Huang Guoping, and Anthony Hays. "Design of hypersonic forebody with submerged bump." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 9 (August 16, 2018): 3153–69. http://dx.doi.org/10.1177/0954410018793288.
Повний текст джерелаCao, Yu Ji, Shi Ying Zhang, and Peng Gao. "Investigation of Attack Angle Character for Hypersonic Inlet." Advanced Materials Research 468-471 (February 2012): 1978–81. http://dx.doi.org/10.4028/www.scientific.net/amr.468-471.1978.
Повний текст джерелаReddy, P. Nithish. "Hypersonic Scram-Jet Engine Inlet Design." International Journal for Research in Applied Science and Engineering Technology 7, no. 6 (June 30, 2019): 1619–35. http://dx.doi.org/10.22214/ijraset.2019.6273.
Повний текст джерелаTeng, Jian, and Hua Cheng Yuan. "Design Methodology and Unsteady Aerodynamic Characteristics of a Rectangular Variable Geometry Hypersonic Inlet." Applied Mechanics and Materials 275-277 (January 2013): 433–41. http://dx.doi.org/10.4028/www.scientific.net/amm.275-277.433.
Повний текст джерелаLi, Yuling, Lianjie Yue, Chengming He, Wannan Wu, and Hao Chen. "Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints." Aerospace 9, no. 10 (October 20, 2022): 625. http://dx.doi.org/10.3390/aerospace9100625.
Повний текст джерелаHe, Xuzhao, Jialing Le, and Si Qin. "Design and analysis osculating general curved cone waverider." Aircraft Engineering and Aerospace Technology 89, no. 6 (October 2, 2017): 797–803. http://dx.doi.org/10.1108/aeat-12-2014-0214.
Повний текст джерелаChang, Juntao, Lei Wang, and Wen Bao. "Mathematical modeling and characteristic analysis of scramjet buzz." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 228, no. 13 (January 29, 2014): 2542–52. http://dx.doi.org/10.1177/0954410014521055.
Повний текст джерелаYan, Yilun, and Jiangfeng Wang. "Numerical Research on the NS-SDBD Control of a Hypersonic Inlet in Off-Design Mode." Aerospace 9, no. 12 (November 30, 2022): 773. http://dx.doi.org/10.3390/aerospace9120773.
Повний текст джерелаXiong, Bing, Xiao-qiang Fan, and Yi Wang. "Parameterization and optimization design of a hypersonic inward turning inlet." Acta Astronautica 164 (November 2019): 130–41. http://dx.doi.org/10.1016/j.actaastro.2019.07.004.
Повний текст джерелаZhu, Chengxiang, Rijiong Yang, Rongqian Chen, Ruofan Qiu, and Yancheng You. "Investigation of adaptive slot control method for starting characteristics of hypersonic inlets." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 11 (December 25, 2018): 4261–71. http://dx.doi.org/10.1177/0954410018819523.
Повний текст джерелаYu, Zonghan, Guoping Huang, Ruilin Wang, and Omer Musa. "Spillage-Adaptive Fixed-Geometry Bump Inlet of Wide Speed Range." Aerospace 8, no. 11 (November 11, 2021): 340. http://dx.doi.org/10.3390/aerospace8110340.
Повний текст джерелаXu, Shang-cheng, Yi Wang, Zhen-guo Wang, Xiao-qiang Fan, and Bing Xiong. "Design method for hypersonic bump inlet based on transverse pressure gradient." Journal of Zhejiang University-SCIENCE A 23, no. 6 (June 2022): 479–94. http://dx.doi.org/10.1631/jzus.a2100532.
Повний текст джерелаKline, H. L., and J. J. Alonso. "Adjoint of Generalized Outflow-Based Functionals Applied to Hypersonic Inlet Design." AIAA Journal 55, no. 11 (November 2017): 3903–15. http://dx.doi.org/10.2514/1.j055863.
Повний текст джерелаYou, YanCheng, and DeWang Liang. "Design concept of three-dimensional section controllable internal waverider hypersonic inlet." Science in China Series E: Technological Sciences 52, no. 7 (June 9, 2009): 2017–28. http://dx.doi.org/10.1007/s11431-009-0125-1.
Повний текст джерелаWang, Jifei, Jinsheng Cai, Yanhui Duan, and Yuan Tian. "Design of shape morphing hypersonic inward-turning inlet using multistage optimization." Aerospace Science and Technology 66 (July 2017): 44–58. http://dx.doi.org/10.1016/j.ast.2017.02.018.
Повний текст джерелаSubbarao, Kamesh, and Jennifer D. Goss. "Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet." International Journal of Aerospace Engineering 2009 (2009): 1–12. http://dx.doi.org/10.1155/2009/793647.
Повний текст джерелаWang, Fang, and Shuang Lin Gao. "Numerical Study on Aerodynamic Design of Hypersonic Vehicle Forebody." Advanced Materials Research 756-759 (September 2013): 4626–29. http://dx.doi.org/10.4028/www.scientific.net/amr.756-759.4626.
Повний текст джерелаZhu, Chengxiang, Xu Zhang, Fan Kong, and Yancheng You. "Design of a Three-Dimensional Hypersonic Inward-Turning Inlet with Tri-Ducts for Combined Cycle Engines." International Journal of Aerospace Engineering 2018 (November 27, 2018): 1–10. http://dx.doi.org/10.1155/2018/7459141.
Повний текст джерелаDing, F., J. Liu, W. Huang, C. Peng, and S. Chen. "An airframe/inlet integrated full-waverider vehicle design using as upgraded aerodynamic method." Aeronautical Journal 123, no. 1266 (June 21, 2019): 1135–69. http://dx.doi.org/10.1017/aer.2019.49.
Повний текст джерелаXU, Shangcheng, Yi WANG, Zhenguo WANG, Xiaoqiang FAN, and Xingyu ZHAO. "Design and analysis of a hypersonic inlet with an integrated bump/forebody." Chinese Journal of Aeronautics 32, no. 10 (October 2019): 2267–74. http://dx.doi.org/10.1016/j.cja.2019.04.010.
Повний текст джерелаDe Vanna, Francesco, Danilo Bof, and Ernesto Benini. "Multi-Objective RANS Aerodynamic Optimization of a Hypersonic Intake Ramp at Mach 5." Energies 15, no. 8 (April 12, 2022): 2811. http://dx.doi.org/10.3390/en15082811.
Повний текст джерелаSarosh, Ali, Dong Yun-Feng, and Muhammad Shoaib. "An Aerothermodynamic and Mass-Model Integrated Optimization Framework for Highly-Integrated Forebody-Inlet Configurations." Applied Mechanics and Materials 245 (December 2012): 277–82. http://dx.doi.org/10.4028/www.scientific.net/amm.245.277.
Повний текст джерелаMiao, Hai Feng, Lv Rong Xie, and Weng Xiao Chai. "Effects of Unforced Bounday Layer Transition on the Performance of a Two-Dimensional Hypersonic Inlet." Applied Mechanics and Materials 275-277 (January 2013): 466–71. http://dx.doi.org/10.4028/www.scientific.net/amm.275-277.466.
Повний текст джерелаYu, Zonghan, Huihui Huang, Ruilin Wang, Yuedi Lei, Xueyang Yan, Zikang Jin, Omer Musa, and Guoping Huang. "Effects of Flow Spillage Strategies on the Aerodynamic Characteristics of Diverterless Hypersonic Inlets." Aerospace 9, no. 12 (November 29, 2022): 771. http://dx.doi.org/10.3390/aerospace9120771.
Повний текст джерелаKang, Sang Hun. "Variable Inlet Design for Hypersonic Engines with a Wide Range of Flight Mach Numbers." Journal of the Korean Society of Propulsion Engineers 19, no. 3 (June 1, 2015): 65–72. http://dx.doi.org/10.6108/kspe.2015.19.3.065.
Повний текст джерелаWen, Xun, Jun Liu, Jie Li, Feng Ding, and Zhi-xun Xia. "Design and numerical simulation of a clamshell-shaped inlet cover for air-breathing hypersonic vehicles." Journal of Zhejiang University-SCIENCE A 20, no. 5 (May 2019): 347–57. http://dx.doi.org/10.1631/jzus.a1800620.
Повний текст джерелаVeeran, Sasha, Apostolos Pesyridis, and Lionel Ganippa. "Ramjet Compression System for a Hypersonic Air Transportation Vehicle Combined Cycle Engine." Energies 11, no. 10 (September 25, 2018): 2558. http://dx.doi.org/10.3390/en11102558.
Повний текст джерелаJi, Zifei, Huiqiang Zhang, and Bing Wang. "Thrust control strategy based on the minimum combustor inlet Mach number to enhance the overall performance of a scramjet engine." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 13 (February 20, 2019): 4810–24. http://dx.doi.org/10.1177/0954410019830816.
Повний текст джерелаUtomo, Muhammad Adnan, and Romie Oktavianus Bura. "Design of Inward-Turning External Compression Supersonic Inlet for Supersonic Transport Aircraft." INSIST 2, no. 2 (January 25, 2019): 104. http://dx.doi.org/10.23960/ins.v2i2.90.
Повний текст джерелаDing, Feng, Jun Liu, Chi-bing Shen, Wei Huang, Zhen Liu, and Shao-hua Chen. "An overview of waverider design concept in airframe/inlet integration methodology for air-breathing hypersonic vehicles." Acta Astronautica 152 (November 2018): 639–56. http://dx.doi.org/10.1016/j.actaastro.2018.09.002.
Повний текст джерелаSarosh, Ali, Dong Yun Feng, and Muhammad Adnan. "An Aerothermodynamic Design Approach for Scramjet Combustors and Comparative Performance of Low-Efficiency Systems." Applied Mechanics and Materials 110-116 (October 2011): 4652–60. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.4652.
Повний текст джерелаWang, Chengpeng, Xin Yang, Longsheng Xue, Konstantinos Kontis, and Yun Jiao. "Correlation Analysis of Separation Shock Oscillation and Wall Pressure Fluctuation in Unstarted Hypersonic Inlet Flow." Aerospace 6, no. 1 (January 10, 2019): 8. http://dx.doi.org/10.3390/aerospace6010008.
Повний текст джерелаWood, J. R., J. F. Schmidt, R. J. Steinke, R. V. Chima, and W. G. Kunik. "Application of Advanced Computational Codes in the Design of an Experiment for a Supersonic Throughflow Fan Rotor." Journal of Turbomachinery 110, no. 2 (April 1, 1988): 270–79. http://dx.doi.org/10.1115/1.3262191.
Повний текст джерелаNavó, Àlex, and Josep M. Bergada. "Aerodynamic Study of the NASA’s X-43A Hypersonic Aircraft." Applied Sciences 10, no. 22 (November 19, 2020): 8211. http://dx.doi.org/10.3390/app10228211.
Повний текст джерелаAl-Garni, A. Z., A. Z. Şahin, and B. S. Yilbas. "Active Cooling of a Hypersonic Plane Using Hydrogen, Methane, Oxygen and Fluorine." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 210, no. 1 (January 1996): 9–17. http://dx.doi.org/10.1243/pime_proc_1996_210_340_02.
Повний текст джерелаFan, Y., J. Chang, W. Bao, and D. Yu. "Effects of boundary-layer bleeding on unstart oscillatory flow of hypersonic inlets." Aeronautical Journal 114, no. 1157 (July 2010): 445–50. http://dx.doi.org/10.1017/s0001924000003924.
Повний текст джерелаLin, Sheam-Chyun, and Yu-Shan Luo. "Integrated design of hypersonic waveriders including inlets and tailfins." Journal of Spacecraft and Rockets 32, no. 1 (January 1995): 48–54. http://dx.doi.org/10.2514/3.26573.
Повний текст джерелаShukla, Vijay, Andrew Gelsey, Mark Schwabacher, Donald Smith, and Doyle D. Knight. "Automated Design Optimization for the P2 and P8 Hypersonic Inlets." Journal of Aircraft 34, no. 2 (March 1997): 228–35. http://dx.doi.org/10.2514/2.2161.
Повний текст джерелаRaj, N. Om Prakash, and K. Venkatasubbaiah. "A new approach for the design of hypersonic scramjet inlets." Physics of Fluids 24, no. 8 (August 2012): 086103. http://dx.doi.org/10.1063/1.4748130.
Повний текст джерелаGollan, Rowan J., and Michael K. Smart. "Design of Modular Shape-Transition Inlets for a Conical Hypersonic Vehicle." Journal of Propulsion and Power 29, no. 4 (July 2013): 832–38. http://dx.doi.org/10.2514/1.b34672.
Повний текст джерелаWang, Chengpeng, Xuang Tian, Lingfeng Yan, Longsheng Xue, and Keming Cheng. "Preliminary Integrated Design of Hypersonic Vehicle Configurations Including Inward-Turning Inlets." Journal of Aerospace Engineering 28, no. 6 (November 2015): 04014143. http://dx.doi.org/10.1061/(asce)as.1943-5525.0000480.
Повний текст джерелаLu, H., and D. Cao. "Three-dimensional design and numerical simulation of magnetohydrodynamic controlled hypersonic inlets." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 226, no. 8 (October 13, 2011): 1002–13. http://dx.doi.org/10.1177/0954410011416059.
Повний текст джерелаSmart, M. K. "Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition." Journal of Propulsion and Power 15, no. 3 (May 1999): 408–16. http://dx.doi.org/10.2514/2.5459.
Повний текст джерелаWANG, Jifei, Jinsheng CAI, Chuanzhen LIU, Yanhui DUAN, and Yaojie YU. "Aerodynamic configuration integration design of hypersonic cruise aircraft with inward-turning inlets." Chinese Journal of Aeronautics 30, no. 4 (August 2017): 1349–62. http://dx.doi.org/10.1016/j.cja.2017.05.002.
Повний текст джерелаCui, Kai, ShouChao Hu, GuangLi Li, ZhiPeng Qu, and Ming Situ. "Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets." Science China Technological Sciences 56, no. 8 (June 28, 2013): 1980–88. http://dx.doi.org/10.1007/s11431-013-5288-0.
Повний текст джерелаFu, Lei, Shuai Zhang, and Yao Zheng. "Performances analysis of asymmetric minimum length nozzles." International Journal of Modeling, Simulation, and Scientific Computing 07, no. 02 (June 2016): 1650021. http://dx.doi.org/10.1142/s1793962316500215.
Повний текст джерелаKovalchuk, O., O. Skorohvatov, A. Galkin, L. Gordishevski, and V. Liskovchuk. "ARMORED SHELLS WITH STRAIGHT AIR JET ENGINE." Collection of scientific works of Odesa Military Academy 1, no. 13 (December 30, 2020): 34–43. http://dx.doi.org/10.37129/2313-7509.2020.13.1.34-43.
Повний текст джерелаBrahmachary, Shuvayan, Ganesh Natarajan, Vinayak Kulkarni, and Niranjan Sahoo. "Comment on “A new approach for the design of hypersonic scramjet inlets” [Phys. Fluids 24, 086103 (2012)]." Physics of Fluids 32, no. 7 (July 1, 2020): 079101. http://dx.doi.org/10.1063/5.0006408.
Повний текст джерелаPrakash Raj, N. Om, and K. Venkatasubbaiah. "Response to “Comment on ‘A new approach for the design of hypersonic scramjet inlets’” [Phys. Fluids 32, 079101 (2020)]." Physics of Fluids 32, no. 7 (July 1, 2020): 079102. http://dx.doi.org/10.1063/5.0012513.
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