Auswahl der wissenschaftlichen Literatur zum Thema „Supersonic / hypersonic“
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Zeitschriftenartikel zum Thema "Supersonic / hypersonic"
Yang, Lung-Jieh, und Chao-Kang Feng. „A Unified Asymptotic Theory of Supersonic, Transonic, and Hypersonic Far Fields“. Axioms 11, Nr. 11 (19.11.2022): 656. http://dx.doi.org/10.3390/axioms11110656.
Der volle Inhalt der QuelleLi, Yong Hong, Xin Wu Tang und Wei Qun Zhou. „Aerodynamic and Numerical Study on the Influence of Spike Shapes at Mach 1.5“. Advanced Materials Research 1046 (Oktober 2014): 177–81. http://dx.doi.org/10.4028/www.scientific.net/amr.1046.177.
Der volle Inhalt der Quellede Araujo Martos, João Felipe, Israel da Silveira Rêgo, Sergio Nicholas Pachon Laiton, Bruno Coelho Lima, Felipe Jean Costa und Paulo Gilberto de Paula Toro. „Experimental Investigation of Brazilian 14-X B Hypersonic Scramjet Aerospace Vehicle“. International Journal of Aerospace Engineering 2017 (2017): 1–10. http://dx.doi.org/10.1155/2017/5496527.
Der volle Inhalt der QuelleMilthorpe, J. F. „Simulation of supersonic and hypersonic flows“. International Journal for Numerical Methods in Fluids 14, Nr. 3 (15.02.1992): 267–88. http://dx.doi.org/10.1002/fld.1650140303.
Der volle Inhalt der QuelleXiao, Han-shan, Chao Ou, Hong-liang Ji, Zheng-chun He, Ning-yuan Liu und Xian-xu Yuan. „Low-Cost and Aerodynamics-Aim Hypersonic Flight Experiment MF-1“. MATEC Web of Conferences 316 (2020): 04006. http://dx.doi.org/10.1051/matecconf/202031604006.
Der volle Inhalt der QuelleVerhoff, A., und D. Stookesberry. „Prediction of inviscid supersonic/hypersonic aircraft flowfields“. Journal of Aircraft 29, Nr. 4 (Juli 1992): 581–87. http://dx.doi.org/10.2514/3.46205.
Der volle Inhalt der QuelleHuang, Wei, Jun-tao Chang und Li Yan. „Mixing and combustion in supersonic/hypersonic flows“. Journal of Zhejiang University-SCIENCE A 21, Nr. 8 (August 2020): 609–13. http://dx.doi.org/10.1631/jzus.a20mcsf1.
Der volle Inhalt der QuelleHu, Jiasen, und Arthur Rizzi. „Turbulent flow in supersonic and hypersonic nozzles“. AIAA Journal 33, Nr. 9 (September 1995): 1634–40. http://dx.doi.org/10.2514/3.12861.
Der volle Inhalt der QuelleJames, Anthony. „Hot Property“. Aerospace Testing International 2018, Nr. 3 (September 2018): 48–52. http://dx.doi.org/10.12968/s1478-2774(23)50116-2.
Der volle Inhalt der QuelleZhao, Lian Jin, Jia Lin, Jian Hua Wang, Jin Long Peng, De Jun Qu und Lian Zhong Chen. „An Experimental Investigation on Transpiration Cooling for Supersonic Vehicle Nose Cone Using Porous Material“. Applied Mechanics and Materials 541-542 (März 2014): 690–94. http://dx.doi.org/10.4028/www.scientific.net/amm.541-542.690.
Der volle Inhalt der QuelleDissertationen zum Thema "Supersonic / hypersonic"
Higgins, Andrew J. „Investigation of detonation initiation by supersonic blunt bodies /“. Thesis, Connect to this title online; UW restricted, 1996. http://hdl.handle.net/1773/10000.
Der volle Inhalt der QuelleDenman, Paul Ashley. „Experimental study of hypersonic boundary layers and base flows“. Thesis, Imperial College London, 1996. http://hdl.handle.net/10044/1/45466.
Der volle Inhalt der QuelleHunt, David Leslie. „An investigation of supersonic buffet using a Large Eddy Simulation“. Thesis, Queen's University Belfast, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.318735.
Der volle Inhalt der QuelleHusmeier, Frank. „Numerical Investigations of Transition in Hypersonic Flows over Circular Cones“. Diss., The University of Arizona, 2008. http://hdl.handle.net/10150/196123.
Der volle Inhalt der QuelleDel, Rio Francesco. „Distortion mechanism in supersonic combustion ramjet engines“. Master's thesis, Alma Mater Studiorum - Università di Bologna, 2018.
Den vollen Inhalt der Quelle findenFuller, Eric James. „Experimental and computational investigation of helium injection into air at supersonic and hypersonic speeds“. Diss., Virginia Tech, 1992. http://hdl.handle.net/10919/39977.
Der volle Inhalt der QuellePh. D.
Lee, Jaewoo. „Efficient inverse methods for supersonic and hypersonic body design, with low wave drag analysis“. Diss., Virginia Tech, 1991. http://hdl.handle.net/10919/37406.
Der volle Inhalt der QuellePh. D.
Grossman, Peter Michael. „Experimental Investigation of a Flush-Walled, Diamond-Shaped Fuel Injector for High Mach Number Scramjets“. Thesis, Virginia Tech, 2007. http://hdl.handle.net/10919/30974.
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The results of the investigation can be summarized as follows. For the baseline case, the aligned diamond injector penetrated 44% higher into the crossflow than did the round injector. The addition of yaw angle increased the crossflow penetration to 53% higher than the round injector. The aligned diamond injector produced a 34% wider jet than the round injector, while the addition of yaw angle somewhat reduced this widening effect to 26% wider than the round injector. The aligned and yawed diamond injectors exhibited 10% and 15% lower mixing efficiency than the round injector, respectively. The total pressure loss parameter of the aligned diamond was 22% lower than the round injector, while the addition of yaw angle improved the total pressure loss parameter to 34% lower than the round injector. For the lower mass flow (and momentum flux ratio) case, the diamond injector demonstrated 52% higher penetration and a 39% wider plume than the round injector. The mixing efficiency was nearly identical between the two injectors with just a 4% lower mixing efficiency for the diamond injector. The total pressure loss parameter of the diamond injector was 32% lower than round injector. These results confirm the conclusions of earlier, lower free stream Mach number and higher molecular weight injectant, studies that a slender diamond injector provides significant benefits for crossflow penetration and lower total pressure losses.
Master of Science
Schreyer, Anne-Marie [Verfasser]. „Experimental investigations of supersonic and hypersonic shock wave/turbulent boundary layer interactions / Anne-Marie Schreyer“. München : Verlag Dr. Hut, 2013. http://d-nb.info/1045126853/34.
Der volle Inhalt der QuelleRock, Christopher. „Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors“. Diss., Virginia Tech, 2010. http://hdl.handle.net/10919/77208.
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Bücher zum Thema "Supersonic / hypersonic"
Center, Langley Research, Hrsg. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.
Den vollen Inhalt der Quelle findenLakin, William D. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.
Den vollen Inhalt der Quelle findenAnderson, Griffin Y. An outlook on hypersonic flight. New York: AIAA, 1987.
Den vollen Inhalt der Quelle findenNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.
Den vollen Inhalt der Quelle findenNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.
Den vollen Inhalt der Quelle findenMiles, Richard B. Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities. Washington: AIAA, 1992.
Den vollen Inhalt der Quelle findenCenter, Langley Research, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Nonparallel instability of supersonic and hypersonic boundary layers. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Den vollen Inhalt der Quelle findenD, Carboni Jeanne, Supersonic investigation of two dimensional .... und United States. National Aeronautics and Space Administration., Hrsg. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenD, Carboni Jeanne, Supersonic investigation of two dimensional... und United States. National Aeronautics and Space Administration., Hrsg. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenL, Pittman Jimmy, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Hrsg. Aerodynamic characteristics of a distinct wing-body configuration at Mach 6: Experiment, theory, and the hypersonic isolation principle. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Den vollen Inhalt der Quelle findenBuchteile zum Thema "Supersonic / hypersonic"
Ingenito, Antonella. „Design of Supersonic/Hypersonic Vehicles“. In Subsonic Combustion Ramjet Design, 9–17. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-66881-5_3.
Der volle Inhalt der QuelleStemmer, Christian, und Nikolaus A. Adams. „Supersonic and Hypersonic Boundary-Layer Flows“. In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 77–91. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-00262-5_4.
Der volle Inhalt der QuelleVervisch, P., und A. Bourdon. „The Recombination of Ionized Species in Supersonic Flows“. In Molecular Physics and Hypersonic Flows, 525–42. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-0267-1_35.
Der volle Inhalt der QuelleMarcos, T. V. C., D. Romanelli Pinto, G. S. Moura, A. C. Oliveira, J. B. Chanes, P. G. P. Toro und M. A. S. Minucci. „Supersonic Combustion Flow Visualization at Hypersonic Flow“. In 28th International Symposium on Shock Waves, 1041–47. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-25685-1_158.
Der volle Inhalt der QuelleWegener, Peter P. „Toward High Speed: Supersonic and Hypersonic Flight“. In What Makes Airplanes Fly?, 145–66. New York, NY: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_10.
Der volle Inhalt der QuelleWegener, Peter P. „Toward High Speed: Supersonic and Hypersonic Flight“. In What Makes Airplanes Fly?, 169–93. New York, NY: Springer New York, 1997. http://dx.doi.org/10.1007/978-1-4612-2254-5_10.
Der volle Inhalt der QuelleSmits, Alexander J., und M. Pino Martin. „Turbulence in Supersonic and Hypersonic Boundary Layers“. In Solid mechanics and its applications, 221–30. Dordrecht: Springer Netherlands, 2006. http://dx.doi.org/10.1007/978-1-4020-4150-1_21.
Der volle Inhalt der QuelleVerhoff, A., D. C. Stookesberry, B. M. Hopping und T. R. Michal. „Supersonic/Hypersonic Euler Flowfield Prediction Method for Aircraft Configurations“. In Numerical and Physical Aspects of Aerodynamic Flows IV, 189–204. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-662-02643-4_12.
Der volle Inhalt der QuelleRomanelli Pinto, D., T. V. C. Marcos, R. L. M. Alcaide, A. C. Oliveira, J. B. Chanes, P. G. P. Toro und M. A. S. Minucci. „Supersonic Combustion Experimental Investigation at T2 Hypersonic Shock Tunnel“. In 28th International Symposium on Shock Waves, 1049–55. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-25685-1_159.
Der volle Inhalt der QuelleSeror, S., und L. Kosarev. „Turbulence Compressibility Effects for Supersonic and Hypersonic Separated Flows“. In 30th International Symposium on Shock Waves 1, 263–67. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-46213-4_43.
Der volle Inhalt der QuelleKonferenzberichte zum Thema "Supersonic / hypersonic"
MASON, W., und JAEWOO LEE. „On optimal supersonic/hypersonic bodies“. In Flight Simulation Technologies Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-3072.
Der volle Inhalt der QuelleSOBIECZKY, H. „Generic supersonic and hypersonic configurations“. In 9th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3301.
Der volle Inhalt der QuelleYOON, W., und T. CHUNG. „Numerical studies of supersonic/hypersonic combustion“. In 30th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-94.
Der volle Inhalt der QuelleLandon, Mark, Darryl Hall, Jerry Udy und Ernest Perry. „Automatic supersonic/hypersonic aerodynamic shape optimization“. In 12th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-1898.
Der volle Inhalt der QuelleAbouali, Omid, und Goodarz Ahmadi. „Bow Shock Effect on Particle Transport and Deposition in a Hypersonic Impactor“. In ASME/JSME 2003 4th Joint Fluids Summer Engineering Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/fedsm2003-45072.
Der volle Inhalt der QuelleZhang, Chen-an, Zheng-yin Ye und Wei-wei Zhang. „Aeroservoelastic Analysis for Supersonic and Hypersonic Missiles“. In 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-1073.
Der volle Inhalt der QuelleNICKERSON, G., S. DUNN und D. MIGDAL. „Optimized supersonic exhaust nozzles for hypersonic propulsion“. In 24th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3161.
Der volle Inhalt der QuelleArai, Takakage, Sosuke Sugano und Shoji Sakaue. „Interaction between Supersonic Cavity Flow and Streamwise Vortices for Supersonic Mixing Enhancement“. In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3613.
Der volle Inhalt der QuelleThakur, Amit, und Corin Segal. „Flameholding Analyses in Supersonic Flow“. In 12th AIAA International Space Planes and Hypersonic Systems and Technologies. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-6909.
Der volle Inhalt der QuelleAbouali, Omid, und Goodarz Ahmadi. „Numerical Modeling of Upstream Nozzle Effect in Supersonic/Hypersonic Impactors for Nano-Particles“. In ASME 2005 Fluids Engineering Division Summer Meeting. ASMEDC, 2005. http://dx.doi.org/10.1115/fedsm2005-77433.
Der volle Inhalt der QuelleBerichte der Organisationen zum Thema "Supersonic / hypersonic"
Kostoff, Ronald N., Henry J. Eberhart und Darrell R. Toothman. Science and Technology Text Mining: Hypersonic and Supersonic Flow. Fort Belvoir, VA: Defense Technical Information Center, November 2003. http://dx.doi.org/10.21236/ada418717.
Der volle Inhalt der QuelleHerbert, Thorwald. Stability of Boundary Layers at High Supersonic and Hypersonic Speeds. Fort Belvoir, VA: Defense Technical Information Center, Mai 1992. http://dx.doi.org/10.21236/ada250900.
Der volle Inhalt der QuelleLempert, Walter R., und Richard B. Miles. Quantitative Imaging of Time-Evolving Structure for Supersonic and Hypersonic Flows. Fort Belvoir, VA: Defense Technical Information Center, März 1995. http://dx.doi.org/10.21236/ada297721.
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