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Статті в журналах з теми "High speed propulsion"
Blount, Donald L., and Robert J. Bartee. "Design of Propulsion Systems for High-Speed Craft." Marine Technology and SNAME News 34, no. 04 (October 1, 1997): 276–92. http://dx.doi.org/10.5957/mt1.1997.34.4.276.
Повний текст джерелаGlushchenko, M. D., and I. O. Goryunov. "Hybrid Propulsion Unit." World of Transport and Transportation 14, no. 3 (June 28, 2016): 72–79. http://dx.doi.org/10.30932/1992-3252-2016-14-3-6.
Повний текст джерелаSrivastava, Shivank, Brandon M. Taravella, Jonathan R. Eastridge, and Kazim M. Akyuzlu. "Numerical Analysis of the Hydrodynamics of an Anguilliform-Like Propulsor for High Efficiency." Marine Technology Society Journal 56, no. 2 (April 27, 2022): 47–63. http://dx.doi.org/10.4031/mtsj.56.2.3.
Повний текст джерелаLi, Bin Cheng, and Bing Han. "Simulation of the Application of Pneumatic Propulsion Method in Tourist Submarine." Applied Mechanics and Materials 43 (December 2010): 603–9. http://dx.doi.org/10.4028/www.scientific.net/amm.43.603.
Повний текст джерелаGany, Alon. "INNOVATIVE CONCEPTS FOR HIGH-SPEED UNDERWATER PROPULSION." International Journal of Energetic Materials and Chemical Propulsion 17, no. 2 (2018): 83–109. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.2018027877.
Повний текст джерелаKinnas, Spyros A. "An International Consortium on High-Speed Propulsion." Marine Technology and SNAME News 33, no. 03 (July 1, 1996): 203–10. http://dx.doi.org/10.5957/mt1.1996.33.3.203.
Повний текст джерелаLEE, Hsing-Juin, Yow-Jeng JONG, Li-Min CHANG, and Wen-Lin WU. "Propulsion Strategy Analysis of High-Speed Swordfish." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 52, no. 175 (2009): 11–20. http://dx.doi.org/10.2322/tjsass.52.11.
Повний текст джерелаBATRAK, D. V., D. V. NIKUSHCHENKO, and A. P. SENKOV. "Electric propulsion system for high-speed vessels." Elektrotekhnika, no. 11 (2022): 59–64. http://dx.doi.org/10.53891/00135860_2022_11_59.
Повний текст джерелаBai, Hongfen. "Position Estimation of a PMSM in an Electric Propulsion Ship System Based on High-Frequency Injection." Electronics 9, no. 2 (February 6, 2020): 276. http://dx.doi.org/10.3390/electronics9020276.
Повний текст джерелаRosato, Daniel A., Mason Thornton, Jonathan Sosa, Christian Bachman, Gabriel B. Goodwin, and Kareem A. Ahmed. "Stabilized detonation for hypersonic propulsion." Proceedings of the National Academy of Sciences 118, no. 20 (May 10, 2021): e2102244118. http://dx.doi.org/10.1073/pnas.2102244118.
Повний текст джерелаДисертації з теми "High speed propulsion"
Mahmoud, Hany Mostafa Mohamed Elsaid. "High-speed applications for electromagnetic propulsion technology." Thesis, University of Sheffield, 2018. http://etheses.whiterose.ac.uk/21373/.
Повний текст джерелаStanislaw, Gregory Scott. "Utility of the flow substitution principle for high speed propulsion applications." Thesis, Massachusetts Institute of Technology, 1997. http://hdl.handle.net/1721.1/49969.
Повний текст джерелаReardon, Jonathan Paul. "Computational Analysis of Transient Unstart/Restart Characteristics in a Variable Geometry, High-Speed Inlet." Diss., Virginia Tech, 2019. http://hdl.handle.net/10919/95883.
Повний текст джерелаDoctor of Philosophy
Flight at high speeds requires efficient engine operation and performance. As the vehicle traverses through its flight profile, the engine will undergo changes in operating conditions. At high speeds, these changes can lead to significant performance loss and can be detrimental to the vehicle. It is, therefore, important to develop tools for predicting characteristics of the engine and its response to disturbances. Computational Fluid Dynamics is a common method of computing the fluid flow through the engine. However, traditionally, CFD has been applied to predict the static performance of an engine. This work seeks to advance the state of the art by applying CFD to predict the transient response of the engine to changes in operating conditions brought about by a variable geometry inlet with rotating components.
Wilson, Althea Grace. "Numerical study of energy utilization in nozzle/plume flow-fields of high-speed air-breathing vehicles." Diss., Rolla, Mo. : Missouri University of Science and Technology, 2008. http://scholarsmine.mst.edu/thesis/pdf/Wilson_09007dcc804d881b.pdf.
Повний текст джерелаVita. The entire thesis text is included in file. Title from title screen of thesis/dissertation PDF file (viewed April 25, 2008) Includes bibliographical references (p. 57).
Louis, Neven. "Numerical simulations of thedecomposition of a greenpropellant." Thesis, KTH, Mekanik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-250021.
Повний текст джерелаMessali, Amir. "Contribution to Rotor Position and Speed Estimation for Synchronous Machine Drive Using High Frequency Voltage Injection : Application to EV/HEV Powertrains." Thesis, Ecole centrale de Nantes, 2019. http://www.theses.fr/2019ECDN0048.
Повний текст джерелаThis thesis is part of the Renault / Centrale Nantes Chair on improving the performance of electric vehicles (EV / HEV). It is dedicated to the problem of estimating the position / speed of self-sensing permanent magnet synchronous motors (PMSM) without mechanical sensors, using high frequency (HF) signal injection techniques over the full speed range of PMSM. In this context, several contributions have been proposed in the demodulation / signal processing and tracking algorithms parts of HF injection techniques, in order to improve the estimation of the position / speed of the MSAP compared to the existing methods. In the demodulation / signal processing part of the HF injection techniques, the contributions consisted of proposing original solutions making it possible to reduce the filtering effects in the estimation chain and to make the latter independent of the electrical machine parameters. In the tracking part, the contributions mainly concern the use of the function sign of the position error (instead of the position error) as measurement information, to estimate the position, the speed and the acceleration of self-sensing PMSM with firstorder sliding mode observers (conventional, step-by-step and adaptive). The contributions proposed in both parts have the advantages of robustifying the estimation chain by making it independent of electrical and mechanical parameters on the one hand. On the other hand, they allow improving the accuracy and performance of the estimation chain, and therefore the control of self-sensing PMSM, in transient and steady-state phases with an easy tuning method. The estimation methods developed were tested in simulation and experimentation on a test bench of electrical machines. The results obtained made it possible to highlight the performances of these methods in terms of trajectory tracking and robustness over the entire operating range of PMSM self-sensing control
Li, Yi-Shu, and 李易樹. "Propulsion Strategy Analysis of High-Speed Dolphin." Thesis, 2008. http://ndltd.ncl.edu.tw/handle/02135691841804419582.
Повний текст джерела國立中興大學
機械工程學系所
96
Even today academia has not yet been able to grasp the essence of dolphin propulsion strategy. After a 65 million years the cetaceans category evolved a high aspect ratio, light, thin/high tail fin for pushing a large amount of water backward with a small velocity difference in order to achieve a high propulsion efficiency. With streamlined body and muscles as power source basis for propulsion, dolphin can swim up to a maximum speed of about 50 km/hour. Herein we will present the innovative concepts of "kidnapped airfoils" and "circulating horsepower" to illustrate how the high-speed dolphins swim forward with body and tail working like two deformable airfoils tightly linked to utilize their lift forces for each other cleverly to form a "kidnapped airfoils" phenomenon and capture body lift power to compensate most of the body drag power. In this manner the dolphin can greatly enhance its propulsion efficiency to easily exceed 400% or even more, meanwhile it solves the long-plagued perplexity of Gray paradox lasting for more than 70 years.
Wu, Wen-Lin, and 吳汶霖. "Propulsion Strategy Analysis of High-Speed Swordfish." Thesis, 2007. http://ndltd.ncl.edu.tw/handle/27596697375107550894.
Повний текст джерела中興大學
機械工程學系所
95
Fish have appeared since Precambrian about 500 million years ago. Nevertheless, related academia still can not grasp the essence of propulsion strategy of high-speed fish. The swordfish evolve many years to end up with a high-aspect-ratio, light, thin, narrow, and high crescent tail fin for pushing a large amount of water backward with a small velocity difference in order to achieve a high propulsion efficiency. With thin, streamlined ultra-low-resistance fish body and sizable muscles as power source basis for propulsion, the swordfish can reach an awesome maximum speed of 130 km/h as the speed king at sea. In this paper, we will explain the innovative concepts of "kidnapped airfoils" and "circulating horsepower" to illustrate how the high-speed swordfish swim forward in an unsteady but rhythmic manner. With body and tail work like two deformable airfoils tightly linked to utilize their lift forces for each other cleverly to form a "kidnapped airfoils" phenomenon. Moreover, they use the sensitive lateral-line sensor to detect the ambient water pressure and attain the best attack angle in order to capture the rotational power of lift in the lift direction by the special long-evolved skills of "circulating horsepower" to compensate most of the resistance power. This skill thus enhances its propulsion efficiency greatly to easily exceed an astonishing 500 % or even more. Meanwhile, it solves the perplexity of Gray paradox lasting for more than 70 years. While taking a panoramic view of the swordfish’s propulsion strategy, in addition to sighing deeply for its amazing synergy of force / beauty and our luck of unveiling the survival secret of innumerable long-evolving fish, we can not help but feel a little bit of sensation regarding this academic Eureka!
Yu, Yuan Hua, and 余遠華. "Discussion on propulsion system for high-speed vehicles." Thesis, 1995. http://ndltd.ncl.edu.tw/handle/90315456633767683334.
Повний текст джерелаMa, Fong-Yuan, and 馬豐源. "Modeling Fatigue Life Reliability Analysis for the Propulsion Shafting of High-speed Vessel." Thesis, 2007. http://ndltd.ncl.edu.tw/handle/29492258697090045160.
Повний текст джерела國立臺灣海洋大學
系統工程暨造船學系
96
In Taiwan, the material of stainless steel SUS630 is usually used in propulsion shafting system for high-speed crafts. Unfortunately, the pitting corrosion will be a main factor to effect the fatigue life cycle of the stainless alloy SUS630. In this study, the prediction model of the residual fatigue life cycle and the reliability have been established under the pitting corrosion condition for the propulsion shafting system of high-speed crafts. In this study, the growth rate and tendency of pitting corrosion occurred in the stainless steel SUS630 specimen is estimated by the grey system theory through the ferric chloride acceleration corrosion test. Under such pitting corrosions, the prediction model of fatigue life has carried out by the results of the rotation bending tests on a set of specimen. Meanwhile, the constants of fatigue crack growth rate of SUS630 under pitting corrosions have been determined by means of the metallurgical graphs by SEM and the fracture surface analysis techniques. In the consequence of these processes, the residual fatigue life and the reliability of a pitting corroded stainless steel shaft can be assessed. From the results of the pitting corrosion experiment, the tendency of growth rate of pitting corrosion of the SUS630 steel is pertaining to an exponential function with time. Based on the results of fatigue tests on the specimen with pitting corrosions, the residual fatigue life cycle is only 10-20% of that of the uncorroded specimen. By the fracture surface analyses of the SEM graphs, it has shown that the direction of fatigue crack propagation between the stages of crack propagation and abrupt fracture has only a 45° angle of change. In use of the Paris formula, the value of Δk is rated between 26 to 46, the material constants n is determined to be 3 and c is 4.4×10-15 for the stainless steel SUS630 shaft material. The established model in the thesis can be applied to the preliminary design for propulsion shaft under the prescribed reliability index and estimate the allowable limitation of pitting corrosion depth and the residual fatigue life. Meanwhile, in the survey stage, this reliability model can be also applied to ascertain whether the shaft should be repaired or not, once the pitting corrosion depth is measured. Thus, the life cycle reliability and safety of the propulsion shaft system can be envisaged. Key words: propulsion shafting system of high-speed craft, stainless steel SUS630, grey system theory, corrosion fatigue and reliability
Книги з теми "High speed propulsion"
Archer, R. Douglas. Introduction to aerospace propulsion. Upper Saddle River, N.J: Prentice Hall, 1996.
Знайти повний текст джерелаB, Murthy S. N., Breugelmans F. A. E, and Von Karman Institute for Fluid Dynamics., eds. High speed propulsion: January 26-29, 1998. Rhode St. Genèse, Belgium: Von Karman Institute for Fluid Dynamics, 1998.
Знайти повний текст джерелаMaido, Saarlas, ed. An introduction to aerospace propulsion. Upper Saddle River, N.J: Prentice Hall, 1996.
Знайти повний текст джерелаHartley, T. T. A hierarchy for modeling high speed propulsion systems. [Washington, DC: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаTimnat, Y. M. Advanced airbreathing propulsion. Malabar, Fla: Krieger Pub. Co., 1996.
Знайти повний текст джерелаRay, J. K. High-speed civil transport flight- and propulsion-control technological issues. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.
Знайти повний текст джерелаRay, J. K. High-speed civil transport flight- and propulsion-control technological issues. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.
Знайти повний текст джерелаShaw, Robert J. Engine technology challenges for a 21st century high speed civil transport. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаShaw, Robert J. Progress toward meeting the propulsion technology challenges for a 21st century high-speed civil transport. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаShaw, Robert J. Progress toward meeting the propulsion technology challenges for a 21st century high-speed civil transport. [Washington, D.C: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаЧастини книг з теми "High speed propulsion"
Yun, Liang, Alan Bliault, and Huan Zong Rong. "Propulsion and Appendages." In High Speed Catamarans and Multihulls, 477–533. New York, NY: Springer New York, 2018. http://dx.doi.org/10.1007/978-1-4939-7891-5_11.
Повний текст джерелаRadojčić, Dejan, Milan Kalajdžić, and Aleksandar Simić. "Additional Topics on Resistance, Propulsion and Powering." In Power Prediction Modeling of Conventional High-Speed Craft, 209–52. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-30607-6_10.
Повний текст джерелаVaisakh, S., and T. M. Muruganandam. "Alternate Schlieren Techniques in High-Speed Flow Visualization." In Proceedings of the National Aerospace Propulsion Conference, 349–56. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-5039-3_20.
Повний текст джерелаKailasanath, K. "Towards Credible CFD Analysis of High-Speed Propulsion Systems." In Sustainable Development for Energy, Power, and Propulsion, 3–13. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-5667-8_1.
Повний текст джерелаMcDaniel, J. C., S. D. Hollo, and K. G. Klavuhn. "Planar Velocimetry in High-Speed Aerodynamic and Propulsion Flowfields." In New Trends in Instrumentation for Hypersonic Research, 381–90. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-011-1828-6_35.
Повний текст джерелаChakraborty, Debasis. "CFD Methods in High-Speed Airbreathing Missile Propulsion Design." In Innovations in Sustainable Energy and Cleaner Environment, 263–91. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-9012-8_12.
Повний текст джерелаKumari, Poonam, V. Prabakar, and A. N. Vishwanatha Rao. "Development Strategy for Evaluating Gas Turbine Driven High-speed Alternator." In Proceedings of the National Aerospace Propulsion Conference, 191–98. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2378-4_12.
Повний текст джерелаWang, Xiaonong, Jingyu Huang, and Zhihong Fang. "Research on EDS Propulsion Characteristics of Superconducting High Speed Maglev Train." In Proceedings of the 5th International Conference on Electrical Engineering and Information Technologies for Rail Transportation (EITRT) 2021, 20–28. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-9905-4_3.
Повний текст джерелаMoríñigo, José A., and José Hermida-Quesada. "Simulation of High-Speed Flow in μ-Rockets for Space Propulsion Applications." In IUTAM Symposium on Advances in Micro- and Nanofluidics, 175–89. Dordrecht: Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-2626-2_14.
Повний текст джерелаIyengar, Venkat S., K. Sathiyamoorthy, J. Srinivas, P. Pratheesh Kumar, and P. Manjunath. "Measurements of Droplet Velocity Fields in Sprays from Liquid Jets Injected in High-Speed Crossflows Using PIV." In Proceedings of the National Aerospace Propulsion Conference, 93–102. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-5039-3_5.
Повний текст джерелаТези доповідей конференцій з теми "High speed propulsion"
WARD, B., and F. HEWITT. "High speed airbreathing propulsion." In 24th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3069.
Повний текст джерелаRUTHERFORD, JOHN, and ROBERT FITZPATRICK. "High-speed rotorcraft propulsion." In 27th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-2147.
Повний текст джерелаSMITH, JR., MARTIN. "21st century high speed transport propulsion." In 24th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2987.
Повний текст джерелаBETTNER, J., R. YOUNT, T. RONAN, and D. PESETSKY. "High speed rotorcraft propulsion system studies." In 27th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-2150.
Повний текст джерелаCONWAY, SCOTT. "Conclusions from high-speed rotorcraft studies." In 27th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-2149.
Повний текст джерелаBETTNER, J., J. HAWKINS, and C. BLANDFORD. "High speed rotorcraft propulsion concepts to control power/speed characteristics." In 28th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3367.
Повний текст джерелаGilkey, S. C., R. H. Hines, and R. J. Shaw. "High Speed Civil Transport Propulsion Installation Issues." In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/95-gt-340.
Повний текст джерелаSmith, Martin G. "HIGH SPEED CIVIL TRANSPORT Propulsion System Studies." In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1990. http://dx.doi.org/10.4271/901891.
Повний текст джерела"Neutron and high speed photogrammetric arcjet diagnosis." In 25th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2955.
Повний текст джерелаHONG, ZUU-CHANG, and C. TAO. "High speed flow over rearward facing step." In 24th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2909.
Повний текст джерелаЗвіти організацій з теми "High speed propulsion"
Bruno, Claudio, and Domenico Simone. LiH as Fuel for High Speed Propulsion. Fort Belvoir, VA: Defense Technical Information Center, October 2011. http://dx.doi.org/10.21236/ada552647.
Повний текст джерелаMartin, R. A., M. A. Merrigan, M. G. Elder, J. T. Sena, E. S. Keddy, and C. C. Silverstein. Heat pipe radiation cooling (HPRC) for high-speed aircraft propulsion. Phase 2 (feasibility) final report. Office of Scientific and Technical Information (OSTI), March 1994. http://dx.doi.org/10.2172/10150250.
Повний текст джерелаCusanelli, Dominic S., and Jonathan Slutsky. Resistance and Stock Propulsion on the High Speed Sealift (HSS) Hybrid Contra-Rotating Shaft-Pod (HCRSP) Concept, Model 5653-3A. Fort Belvoir, VA: Defense Technical Information Center, September 2008. http://dx.doi.org/10.21236/ada487320.
Повний текст джерелаAnalysis of Recompression-Regeneration sCO 2 Combined Cycle Utilizing Marine Gas Turbine Exhaust Heat: Effect of Operating Parameters. SAE International, July 2022. http://dx.doi.org/10.4271/2022-01-5059.
Повний текст джерела