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Статті в журналах з теми "Supersonic diffuser"
Wen, Chuang, Xue Wen Cao, Bin Yan, and Jing Zhang. "Optimization Design of Diffusers for Supersonic Separators." Applied Mechanics and Materials 44-47 (December 2010): 1913–17. http://dx.doi.org/10.4028/www.scientific.net/amm.44-47.1913.
Повний текст джерелаLi, Qingkuo, Zhigang Sun, Xingen Lu, Yingjie Zhang, and Ge Han. "Investigation of New Design Principles for the Centrifugal Compressor Vaned Diffusers." International Journal of Aerospace Engineering 2022 (February 25, 2022): 1–16. http://dx.doi.org/10.1155/2022/4480676.
Повний текст джерелаFarahat, Said, Seyyed Morteza Javadpour, Hesamodin Ebnodin Hamidi, and Ebrahim Kadivar. "Optimization of a supersonic wind tunnel diffuser using genetic algorithm." Engineering Computations 32, no. 6 (August 3, 2015): 1691–707. http://dx.doi.org/10.1108/ec-04-2014-0077.
Повний текст джерелаBiedron, R. T., and T. C. Adamson. "Unsteady flow in a supercritical supersonic diffuser." AIAA Journal 26, no. 11 (November 1988): 1336–45. http://dx.doi.org/10.2514/3.10045.
Повний текст джерелаMatsuo, T., M. Ishikawa, and J. Umoto. "Numerical analysis of bifurcation phenomena in supersonic MHD generator with supersonic diffuser." Energy Conversion and Management 35, no. 6 (June 1994): 507–16. http://dx.doi.org/10.1016/0196-8904(94)90092-2.
Повний текст джерелаJo, Seonghwi, Sanghyeon Han, Hong Jip Kim, and Kyung Jin Yim. "Numerical Study on the Flow and Heat Transfer Characteristics of a Second Throat Exhaust Diffuser According to Variations in Operating Pressure and Geometric Shape." Energies 14, no. 3 (January 20, 2021): 532. http://dx.doi.org/10.3390/en14030532.
Повний текст джерелаPapamoschou, Dimitri. "Diffuser performance of two-stream supersonic wind tunnels." AIAA Journal 27, no. 8 (August 1989): 1124–27. http://dx.doi.org/10.2514/3.10232.
Повний текст джерелаSaravanan, G., Ravichandra Kumar, and A. Vinoth Kumar. "Performance Analysis of a Two-Dimensional Supersonic Diffuser." Journal of Advances in Mechanical Engineering and Science 2, no. 2 (April 30, 2016): 42–53. http://dx.doi.org/10.18831/james.in/2016021004.
Повний текст джерелаSinghal, Gaurav, Mainuddin, R. Rajesh, R. K. Tyagi, and A. L. Dawar. "Supersonic diffuser for pressure recovery in SCOIL system." Optics & Laser Technology 42, no. 1 (February 2010): 219–24. http://dx.doi.org/10.1016/j.optlastec.2009.06.009.
Повний текст джерелаPuzach, S. V. "Effect of supersonic diffuser geometry on operation conditions." Experimental Thermal and Fluid Science 5, no. 1 (January 1992): 124–28. http://dx.doi.org/10.1016/0894-1777(92)90061-9.
Повний текст джерелаДисертації з теми "Supersonic diffuser"
Zebiri, Boubakr. "Étude numérique des interactions onde de choc / couche limite dans les tuyères propulsives Shock-induced flow separation in an overexpanded supersonic planar nozzle A parallel high-order compressible flows solver with domain decomposition method in the generalized curvilinear coordinates system Analysis of shock-wave unsteadiness in conical supersonic nozzles." Thesis, Normandie, 2020. http://www.theses.fr/2020NORMIR06.
Повний текст джерелаThe need for a better understanding of the driving mechanism for the observed low-frequency unsteadiness in an over-expanded nozzle flows was discussed. The unsteady character of the shock wave/boundary layer remains an important practical challenge for the nozzle flow problems. Additionally, for a given incoming turbulent boundary layer, this kind of flow usually exhibits higher low-frequency shock motions which are less coupled from the timescales of the incoming turbulence. This may be good from an experimenter’s point of view, because of the difficulties in measuring higher frequencies, but it is more challenging from a computational point of view due to the need to obtain long time series to resolve low-frequency movements. In excellent agreement with the experimental findings, a very-long LES simulation run was carried out to demonstrate the existence of energetic broadband low-frequency motions near the separation point. Particular efforts were done in order to avoid any upstream low-frequency forcing, and it was explicitly demonstrated that the observed low-frequency shock oscillations were not connected with the inflow turbulence generation, ruling out the possibility of a numerical artefact. Different methods of spectral analysis and dynamic mode decomposition have been used to show that the timescales involved in such a mechanism are about two orders of magnitude larger than the time scales involved in the turbulence of the boundary layer, which is consistent with the observed low-frequency motions. Furthermore, those timescales were shown to be strongly modulated by the amount of reversed flow inside the separation bubble. This scenario can, in principle, explain both the low-frequency unsteadiness and its broadband nature
Ghosh, Somnath [Verfasser]. "Direct and large eddy simulation of supersonic turbulent flow in pipes, nozzles and diffusers / Somnath Ghosh." 2008. http://d-nb.info/98843394X/34.
Повний текст джерелаКниги з теми "Supersonic diffuser"
L, Burley Richard, Johns Albert L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Analytical and experimental studies of a short compact subsonic diffuser for a two-dimensional supersonic inlet. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Знайти повний текст джерелаA full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаA full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаH, Anderson Bernhard, Shaw Robert J. 1946-, and United States. National Aeronautics and Space Administration., eds. A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаH, Anderson Bernhard, Shaw Robert J. 1946-, and United States. National Aeronautics and Space Administration., eds. A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаAndreja, Brankovic, and NASA Glenn Research Center, eds. Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Analytical and Experimental Studies of a Short Compact Subsonic Diffuser for a Two-Dimensional Supersonic Inlet. Independently Published, 2018.
Знайти повний текст джерелаD, Saunders J., and United States. National Aeronautics and Space Administration., eds. Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаParametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаD, Saunders J., and United States. National Aeronautics and Space Administration., eds. Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаЧастини книг з теми "Supersonic diffuser"
James, Jintu K., and T. M. Muruganandam. "Shock Oscillations in a Supersonic Diffuser Flow with Varying Stagnation Pressure." In 31st International Symposium on Shock Waves 2, 829–35. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91017-8_103.
Повний текст джерелаGhosh, Somnath, and Rainer Friedrich. "On the Turbulence Structure in a Supersonic Diffuser with Circular Cross-Section." In High Performance Computing in Science and Engineering, Garching/Munich 2009, 89–97. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-13872-0_8.
Повний текст джерелаManoj Prabakar, S., and T. M. Muruganandam. "Experimental Investigations of a Diffuser Start/Unstart Characteristics for Two Stream Supersonic Wind Tunnel." In 31st International Symposium on Shock Waves 2, 1119–26. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91017-8_139.
Повний текст джерелаCastañeda, Héctor O. "Supersonic Turbulence in Giant Extragalactic HII Regions." In Kinematics and Dynamics of Diffuse Astrophysical Media, 285–89. Dordrecht: Springer Netherlands, 1994. http://dx.doi.org/10.1007/978-94-011-0926-0_46.
Повний текст джерелаMalone, M. T., J. E. Dyson, and T. W. Hartquist. "Highly Supersonic Molecular Flows in Wind-Clump Boundary Layers." In Kinematics and Dynamics of Diffuse Astrophysical Media, 143–50. Dordrecht: Springer Netherlands, 1994. http://dx.doi.org/10.1007/978-94-011-0926-0_24.
Повний текст джерелаPrabakar, S. Manoj, Chimakurthy Srikanth, and T. M. Muruganandam. "Effect of Mach Number on Shock Oscillations in Supersonic Diffusers." In 30th International Symposium on Shock Waves 1, 257–61. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-46213-4_42.
Повний текст джерелаAshokkumar, R., Sathiyavageeswaran Sankaran, and T. Sundararajan. "Investigation of Second Throat Supersonic Exhaust Diffusers for the Altitude Testing of Rocket Motors." In Lecture Notes in Mechanical Engineering, 647–55. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-0698-4_71.
Повний текст джерелаGhosh, Somnath, and Rainer Friedrich. "Green's Function Analysis of Pressure-Strain Correlations in a Supersonic Pipe, Nozzle and Diffuser." In Advances in Computation, Modeling and Control of Transitional and Turbulent Flows, 311–20. WORLD SCIENTIFIC, 2015. http://dx.doi.org/10.1142/9789814635165_0030.
Повний текст джерела"Supersonic Diffusers." In Analytical Fluid Dynamics, Third Edition, 343–69. CRC Press, 2015. http://dx.doi.org/10.1201/b19392-21.
Повний текст джерела"18: Supersonic Diffusers." In Analytical Fluid Dynamics, 343–70. 6000 Broken Sound Parkway NW, Suite 300 Boca Raton, FL 33487-2742: CRC Press, 2015. http://dx.doi.org/10.1201/9781315148076-21.
Повний текст джерелаТези доповідей конференцій з теми "Supersonic diffuser"
Gillen, Tyler, Michael Rybalko, and Eric Loth. "Vortex Generators for Diffuser of Axisymmetric Supersonic Inlets." In 5th Flow Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-4253.
Повний текст джерела"Combustion-driven M3 supersonic wind tunnel with diffuser-ejector." In 25th Plasmadynamics and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2573.
Повний текст джерелаSugimoto, Takao, Tsukinami Kawanishi, Hiroshige Kumamaru, and Yasumasa Tohbe. "Performance Investigation Into Supersonic Diffuser for a High Pressure Centrifugal Compressor." In ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/gt2014-25104.
Повний текст джерелаLi, Xiangru, and Feng He. "Periodic Oscillations of Flow Structures in a Supersonic Diffuser Pipe." In 21st AIAA International Space Planes and Hypersonics Technologies Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-2313.
Повний текст джерелаSung, Hong-Gye, Sangkyu Yoon, Hyowon Yeom, Jinkon Kim, Yongwook Kim, Yongsung Ko, Yongwook Kim, and Seunghyup Oh. "Study on Design- and Operation- Parameters of Supersonic Exhaust Diffuser." In 46th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-855.
Повний текст джерелаLee, Sunghun, Myeongwon Lee, Jin Park, and Hongjip Kim. "A Numerical Study on Flow Characteristics of Super Sonic Diffuser for the Position and Nose Cone Angles of Center Body." In ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/ajkfluids2019-5430.
Повний текст джерелаDudek, J., D. Davis, and J. Slater. "Validation and verification of the wind code for supersonic diffuser flow." In 39th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-224.
Повний текст джерелаBurrows, Travis J., Bojan Vukasinovic, and Ari Glezer. "Fluidic Control of an Aggressive Offset Diffuser for a Supersonic Inlet." In 47th AIAA Fluid Dynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4304.
Повний текст джерелаBENSON, RUSTY, and D. MCRAE. "Numerical simulations of the unstart phenomenon in a supersonic inlet/diffuser." In 29th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2239.
Повний текст джерелаOH, JONG, and VIGOR YANG. "Interactions Between Shock and Acoustic Waves in a Supersonic Inlet Diffuser." In 30th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2706.
Повний текст джерела