Artículos de revistas sobre el tema "Rocket engine nozzle"
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Strelnikov, G. A., A. D. Yhnatev, N. S. Pryadko y S. S. Vasyliv. "Gas flow control in rocket engines". Technical mechanics 2021, n.º 2 (29 de junio de 2021): 60–77. http://dx.doi.org/10.15407/itm2021.02.060.
Texto completoJéger, Csaba y Árpád Veress. "Novell Application of CFD for Rocket Engine Nozzle Optimization". Periodica Polytechnica Transportation Engineering 47, n.º 2 (10 de enero de 2018): 131–35. http://dx.doi.org/10.3311/pptr.11490.
Texto completoGuram, Sejal, Vidhanshu Jadhav, Prasad Sawant y Ankit Kumar Mishra. "Review Study on Thermal Characteristics of Bell Nozzle used in Supersonic Engine". 1 2, n.º 1 (1 de marzo de 2023): 4–14. http://dx.doi.org/10.46632/jame/2/1/2.
Texto completoZAGANESCU, Nicolae-Florin, Rodica ZAGANESCU y Constantin-Marcian GHEORGHE. "Wernher Von Braun’s Pioneering Work in Modelling and Testing Liquid-Propellant Rockets". INCAS BULLETIN 14, n.º 2 (10 de junio de 2022): 153–61. http://dx.doi.org/10.13111/2066-8201.2022.14.2.13.
Texto completoBogoi, Alina, Radu D. Rugescu, Valentin Ionut Misirliu, Florin Radu Bacaran y Mihai Predoiu. "Inviscid Nozzle for Aerospike Rocket Engine Application". Applied Mechanics and Materials 811 (noviembre de 2015): 152–56. http://dx.doi.org/10.4028/www.scientific.net/amm.811.152.
Texto completoSultanov, T. S. y G. A. Glebov. "Numerical Computation of Specific Impulse and Internal Flow Parameters in Solid Fuel Rocket Motors with Two-Phase Сombustion Products". Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, n.º 3 (138) (septiembre de 2021): 98–107. http://dx.doi.org/10.18698/0236-3941-2021-3-98-107.
Texto completoBruce Ralphin Rose, J. y J. Veni Grace. "Performance analysis of lobed nozzle ejectors for high altitude simulation of rocket engines". International Journal of Modeling, Simulation, and Scientific Computing 05, n.º 04 (29 de septiembre de 2014): 1450019. http://dx.doi.org/10.1142/s1793962314500196.
Texto completoShustov, S. A., I. E. Ivanov y I. A. Kryukov. "Numerical study of the separation of a turbulent boundary in rocket engine nozzles with an optimized supersonic part". Journal of Physics: Conference Series 2308, n.º 1 (1 de julio de 2022): 012015. http://dx.doi.org/10.1088/1742-6596/2308/1/012015.
Texto completoVasyliv, S. S. y H. O. Strelnykov. "Rocket engine thrust vector control by detonation product injection into the supersonic portion of the nozzle". Technical mechanics 2020, n.º 4 (10 de diciembre de 2020): 29–34. http://dx.doi.org/10.15407/itm2020.04.029.
Texto completoKumar, S. Senthil y M. Arularasu. "Advanced Computational Flow Analysis - Rocket Engine Nozzle". Asian Journal of Research in Social Sciences and Humanities 6, n.º 11 (2016): 1219. http://dx.doi.org/10.5958/2249-7315.2016.01265.x.
Texto completoNae, Catalin, Irina-Carmen Andrei, Gabriela-Liliana Stroe y Sorin Berbente. "Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine�s Bell Exhaust Nozzle and Combustion Chamber". Revista de Chimie 71, n.º 1 (7 de febrero de 2020): 436–44. http://dx.doi.org/10.37358/rc.20.1.7872.
Texto completoO¨stlund, J. y B. Muhammad-Klingmann. "Supersonic Flow Separation with Application to Rocket Engine Nozzles". Applied Mechanics Reviews 58, n.º 3 (1 de mayo de 2005): 143–77. http://dx.doi.org/10.1115/1.1894402.
Texto completoAbada, Omar, Abderahim Abada y Ahmed Abdallah El-Hirtsi. "Effect of bipropellant combustion products on the rocket nozzle design". Mechanics & Industry 21, n.º 5 (2020): 515. http://dx.doi.org/10.1051/meca/2020064.
Texto completoWang, Yan Dong y Hong Guang Jia. "Numerical Simulation of Laval Nozzle". Applied Mechanics and Materials 397-400 (septiembre de 2013): 266–69. http://dx.doi.org/10.4028/www.scientific.net/amm.397-400.266.
Texto completoSellam, Mohamed y Amer Chpoun. "Numerical Simulation of Reactive Flows in Overexpanded Supersonic Nozzle with Film Cooling". International Journal of Aerospace Engineering 2015 (2015): 1–15. http://dx.doi.org/10.1155/2015/252404.
Texto completoZieliński, Mateusz, Piotr Koniorczyk, Janusz Zmywaczyk y Marek Preiskorn. "Numerical simulations of temperature fields in the uncooled nozzle of a short-range anti-aircraft rocket engine with an insert in the critical section made of various materials". Bulletin of the Military University of Technology 70, n.º 1 (31 de marzo de 2021): 15–30. http://dx.doi.org/10.5604/01.3001.0015.6955.
Texto completoSabirzyanov, A. N., A. I. Glazunov, A. N. Kirillova y K. S. Titov. "Simulation of a Rocket Engine Nozzle Discharge Coefficient". Russian Aeronautics 61, n.º 2 (abril de 2018): 257–64. http://dx.doi.org/10.3103/s1068799818020150.
Texto completoSemenov, Vasiliy, Igor Ivanov y Igor Kryukov. "Dual bell slot nozzle of a rocket engine". Perm National Research Polytechnic University Aerospace Engineering Bulletin, n.º 46 (2016): 56–72. http://dx.doi.org/10.15593/2224-9982/2016.46.03.
Texto completoYagodnikov, D. A., A. V. Voronetskii y N. M. Pushkin. "Electrification of nozzle in a liquid rocket engine". Combustion, Explosion, and Shock Waves 31, n.º 4 (1995): 450–54. http://dx.doi.org/10.1007/bf00789365.
Texto completoSun, Dechuan, Tianyou Luo y Qiang Feng. "New Contour Design Method for Rocket Nozzle of Large Area Ratio". International Journal of Aerospace Engineering 2019 (20 de diciembre de 2019): 1–8. http://dx.doi.org/10.1155/2019/4926413.
Texto completoBhupendra Kumar, Mohd Shoaib, Ramanan G y Radhakrishnan P. "Design and Computational Flow Analysis of Different Rocket Nozzle Profile". ACS Journal for Science and Engineering 2, n.º 2 (1 de septiembre de 2022): 49–60. http://dx.doi.org/10.34293/acsjse.v2i2.38.
Texto completoCunningham, Carson F., Mark C. Anderson, Levi T. Moats, Kent L. Gee, Grant W. Hart, Lucas K. Hall y Steven C. Campbell. "Acoustical measurement and analysis of an Atlas V launch without solid rocket boosters". Journal of the Acoustical Society of America 151, n.º 4 (abril de 2022): A83. http://dx.doi.org/10.1121/10.0010730.
Texto completoBrykov, N. A. y K. A. Tischenko. "Computational study of gas flow characteristics when using intra-nozzle interceptors for thrust vector control". Journal of Physics: Conference Series 2388, n.º 1 (1 de diciembre de 2022): 012098. http://dx.doi.org/10.1088/1742-6596/2388/1/012098.
Texto completoLeto, Angelo. "Investigation of a Radial Turbines Compatibility for Small Rocket Engine". E3S Web of Conferences 197 (2020): 11009. http://dx.doi.org/10.1051/e3sconf/202019711009.
Texto completoManski, Detlef y Gerald Hagemann. "Influence of rocket design parameters on engine nozzle efficiencies". Journal of Propulsion and Power 12, n.º 1 (enero de 1996): 41–47. http://dx.doi.org/10.2514/3.23988.
Texto completoCai, Guobiao, Jie Fang, Xu Xu y Minghao Liu. "Performance prediction and optimization for liquid rocket engine nozzle". Aerospace Science and Technology 11, n.º 2-3 (marzo de 2007): 155–62. http://dx.doi.org/10.1016/j.ast.2006.07.002.
Texto completoBennewitz, John W., Blaine R. Bigler, Mathias C. Ross, Stephen A. Danczyk, William A. Hargus y Richard D. Smith. "Performance of a Rotating Detonation Rocket Engine with Various Convergent Nozzles and Chamber Lengths". Energies 14, n.º 8 (7 de abril de 2021): 2037. http://dx.doi.org/10.3390/en14082037.
Texto completoDîrloman, F.-M., L.-C. Matache, T. Rotariu, T.-V. Țigănescu, D. Zvîncu, M.-I. Ungureanu y O. Iorga. "Computational fluid dynamics simulations for composite rocket propellant optimization". IOP Conference Series: Materials Science and Engineering 1182, n.º 1 (1 de octubre de 2021): 012017. http://dx.doi.org/10.1088/1757-899x/1182/1/012017.
Texto completoHasegawa, Keiichi, Akinaga Kumakawa, Kazuo Kusaka, Masahiro Sato, Makoto Tadano, Akira Konno, Hiroshi Aoki, Eijiro Namura y Masahiro Atsumi. "Fundamental Study of Extendible Nozzle and Dual-Bell Nozzle for Reusable Rocket Engine". SPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2 (2003): 25–34. http://dx.doi.org/10.2322/stj.2.25.
Texto completoZhao, Na, Yong Gang Yu y Yu Qiang Wang. "Numerical Simulation of the Spray Characteristics in Small Scale Liquid Rocket Engine Combustion Chamber". Advanced Materials Research 383-390 (noviembre de 2011): 7729–33. http://dx.doi.org/10.4028/www.scientific.net/amr.383-390.7729.
Texto completoLEE, YOUNG-SHIN, JAE-HOON KIM, HYUN-SOO KIM, DUCK-HOI KIM, SEONG-HOI KU y SOON-IL MOON. "A STUDY ON THE THERMAL VIBRATION ANALYSIS OF THE GRAPHITE DISK UNDER THERMAL SHOCK". International Journal of Modern Physics B 20, n.º 25n27 (30 de octubre de 2006): 4105–10. http://dx.doi.org/10.1142/s0217979206040933.
Texto completoArzhannikov, Andrey y Alexey Beklemishev. "An Electro-Jet Rocket Engine With Big Thrust At Helical Corrugated Magnetic Field". Siberian Journal of Physics 11, n.º 1 (1 de marzo de 2016): 107–18. http://dx.doi.org/10.54362/1818-7919-2016-11-1-107-118.
Texto completoZhao, Wei Guo, Ji Hong Dong, Wei Li, Hai Ping Wang y Quan Feng Guo. "Research on Defect Detection Technology of C/C Composite". Advanced Materials Research 295-297 (julio de 2011): 264–69. http://dx.doi.org/10.4028/www.scientific.net/amr.295-297.264.
Texto completoRyzhkov, V. V. y I. I. Morozov. "Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD". VESTNIK of Samara University. Aerospace and Mechanical Engineering 18, n.º 2 (2 de julio de 2019): 62–74. http://dx.doi.org/10.18287/2541-7533-2019-18-2-62-74.
Texto completoVerma, S. B. y Oskar Haidn. "Unsteady Side-Load Evolution in a Liquid Rocket Engine Nozzle". Journal of Spacecraft and Rockets 57, n.º 2 (marzo de 2020): 391–97. http://dx.doi.org/10.2514/1.a34556.
Texto completoForde, Scott, Mel Bulman y Todd Neill. "Thrust augmentation nozzle (TAN) concept for rocket engine booster applications". Acta Astronautica 59, n.º 1-5 (julio de 2006): 271–77. http://dx.doi.org/10.1016/j.actaastro.2006.02.052.
Texto completoVinod, G., S. Renjith y V. Thaddeus Basker. "Thermo Structural Analysis of Carbon-Carbon Nozzle Exit Cone for Rocket Cryo Engines". Applied Mechanics and Materials 877 (febrero de 2018): 320–26. http://dx.doi.org/10.4028/www.scientific.net/amm.877.320.
Texto completoKOSTYUSHIN, Kirill V. "NUMERICAL INVESTIGATION OF UNSTEADY GASDYNAMIC PROCESSES AT THE LAUNCH OF SOLID-PROPELLANT ROCKETS". Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mekhanika, n.º 67 (2020): 127–43. http://dx.doi.org/10.17223/19988621/67/12.
Texto completoMironov, Daniil y Aleksey Salnikov. "DYNAMIC BEHAVIOR OF SOLID FUEL ROCKET ENGINE DURING OPERATION (REVIEW)". Perm National Research Polytechnic University Aerospace Engineering Bulletin, n.º 70 (2022): 7–17. http://dx.doi.org/10.15593/2224-9982/2022.70.01.
Texto completoSomov, V. V. "DETERMINATION OF THE TYPE OF A SINGLE-USE GRENADE LAUNCHER BASED ON ITS COMPOSITE PARTS AND FRAGMENTS OF REACTIVE GRENADE FOUND AT THE PLACE OF ACCIDENT". Theory and Practice of Forensic Science and Criminalistics 17 (29 de noviembre de 2017): 245–52. http://dx.doi.org/10.32353/khrife.2017.31.
Texto completoWolański, P. "RDE research and development in Poland". Shock Waves 31, n.º 7 (octubre de 2021): 623–36. http://dx.doi.org/10.1007/s00193-021-01038-2.
Texto completoBeyer, Steffen, Stephan Schmidt, Franz Maidl, Rolf Meistring, Marc Bouchez y Patrick Peres. "Advanced Composite Materials for Current and Future Propulsion and Industrial Applications". Advances in Science and Technology 50 (octubre de 2006): 174–81. http://dx.doi.org/10.4028/www.scientific.net/ast.50.174.
Texto completoGao, Yuhang y Jian Zheng. "Noise simulation of wake field of solid rocket motor". Journal of Physics: Conference Series 2364, n.º 1 (1 de noviembre de 2022): 012004. http://dx.doi.org/10.1088/1742-6596/2364/1/012004.
Texto completoKhan, Sohaib, Muhammad Umer Sohail, Ihtzaz Qamar, Muzna Tariq y Raees Fida Swati. "Effect of Secondary Combustion on Thrust Regulation of Gas Generator Cycle Rocket Engine". Applied Sciences 12, n.º 20 (19 de octubre de 2022): 10563. http://dx.doi.org/10.3390/app122010563.
Texto completoMosolov, S. V., I. G. Lozino-Lozinskaya, D. M. Pozvonkov y D. F. Slesarev. "Test Results of a Model Additively Manufactured Oxygen-Methane Combustion Chamber of a Liquid Rocket Engine". Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, n.º 3 (138) (septiembre de 2021): 60–79. http://dx.doi.org/10.18698/0236-3941-2021-3-60-79.
Texto completoSimmons, J. y Richard Branam. "Parametric Study of Dual-Expander Aerospike Nozzle Upper-Stage Rocket Engine". Journal of Spacecraft and Rockets 48, n.º 2 (marzo de 2011): 355–67. http://dx.doi.org/10.2514/1.51534.
Texto completoOtsubo, Naoyuki, Kunio Hirata y Hirotaka Otsu. "659 Enhancement of Rocket Engine Thrust using Variable Area Ratio Nozzle". Proceedings of Conference of Tokai Branch 2008.57 (2008): 439–40. http://dx.doi.org/10.1299/jsmetokai.2008.57.439.
Texto completoTrzun, Zvonko, Milan Vrdoljak y Hrvoje Cajner. "The Effect of Manufacturing Quality on Rocket Precision". Aerospace 8, n.º 6 (4 de junio de 2021): 160. http://dx.doi.org/10.3390/aerospace8060160.
Texto completoMa, Yarui, Jiwen Cui, Hui Wang y Jiubin Tan. "Impacts of Micro-Deviations of Aperture on the Characteristics of Collision Atomization Field". Applied Sciences 12, n.º 9 (6 de mayo de 2022): 4685. http://dx.doi.org/10.3390/app12094685.
Texto completoLin, Binbin, Hongliang Pan, Lei Shi y Jinying Ye. "Effect of Primary Rocket Jet on Thermodynamic Cycle of RBCC in Ejector Mode". International Journal of Turbo & Jet-Engines 37, n.º 1 (26 de marzo de 2020): 61–70. http://dx.doi.org/10.1515/tjj-2017-0013.
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