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Artykuły w czasopismach na temat "Supersonic / hypersonic"
Yang, Lung-Jieh, i 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.
Pełny tekst źródłaLi, Yong Hong, Xin Wu Tang i Wei Qun Zhou. "Aerodynamic and Numerical Study on the Influence of Spike Shapes at Mach 1.5". Advanced Materials Research 1046 (październik 2014): 177–81. http://dx.doi.org/10.4028/www.scientific.net/amr.1046.177.
Pełny tekst źródłade Araujo Martos, João Felipe, Israel da Silveira Rêgo, Sergio Nicholas Pachon Laiton, Bruno Coelho Lima, Felipe Jean Costa i 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.
Pełny tekst źródłaMilthorpe, 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.
Pełny tekst źródłaXiao, Han-shan, Chao Ou, Hong-liang Ji, Zheng-chun He, Ning-yuan Liu i 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.
Pełny tekst źródłaVerhoff, A., i D. Stookesberry. "Prediction of inviscid supersonic/hypersonic aircraft flowfields". Journal of Aircraft 29, nr 4 (lipiec 1992): 581–87. http://dx.doi.org/10.2514/3.46205.
Pełny tekst źródłaHuang, Wei, Jun-tao Chang i Li Yan. "Mixing and combustion in supersonic/hypersonic flows". Journal of Zhejiang University-SCIENCE A 21, nr 8 (sierpień 2020): 609–13. http://dx.doi.org/10.1631/jzus.a20mcsf1.
Pełny tekst źródłaHu, Jiasen, i Arthur Rizzi. "Turbulent flow in supersonic and hypersonic nozzles". AIAA Journal 33, nr 9 (wrzesień 1995): 1634–40. http://dx.doi.org/10.2514/3.12861.
Pełny tekst źródłaJames, Anthony. "Hot Property". Aerospace Testing International 2018, nr 3 (wrzesień 2018): 48–52. http://dx.doi.org/10.12968/s1478-2774(23)50116-2.
Pełny tekst źródłaZhao, Lian Jin, Jia Lin, Jian Hua Wang, Jin Long Peng, De Jun Qu i Lian Zhong Chen. "An Experimental Investigation on Transpiration Cooling for Supersonic Vehicle Nose Cone Using Porous Material". Applied Mechanics and Materials 541-542 (marzec 2014): 690–94. http://dx.doi.org/10.4028/www.scientific.net/amm.541-542.690.
Pełny tekst źródłaRozprawy doktorskie na temat "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.
Pełny tekst źródłaDenman, Paul Ashley. "Experimental study of hypersonic boundary layers and base flows". Thesis, Imperial College London, 1996. http://hdl.handle.net/10044/1/45466.
Pełny tekst źródłaHunt, 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.
Pełny tekst źródłaHusmeier, Frank. "Numerical Investigations of Transition in Hypersonic Flows over Circular Cones". Diss., The University of Arizona, 2008. http://hdl.handle.net/10150/196123.
Pełny tekst źródłaDel, Rio Francesco. "Distortion mechanism in supersonic combustion ramjet engines". Master's thesis, Alma Mater Studiorum - Università di Bologna, 2018.
Znajdź pełny tekst źródłaFuller, 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.
Pełny tekst źródłaPh. 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.
Pełny tekst źródłaPh. 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.
Pełny tekst źródła
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.
Pełny tekst źródłaRock, Christopher. "Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors". Diss., Virginia Tech, 2010. http://hdl.handle.net/10919/77208.
Pełny tekst źródłaPh. D.
Książki na temat "Supersonic / hypersonic"
Center, Langley Research, red. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.
Znajdź pełny tekst źródłaLakin, William D. Wave-interactions in supersonic and hypersonic flows. Norfolk, Va: Old Dominion University Research Foundation, 1990.
Znajdź pełny tekst źródłaAnderson, Griffin Y. An outlook on hypersonic flight. New York: AIAA, 1987.
Znajdź pełny tekst źródłaNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.
Znajdź pełny tekst źródłaNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.
Znajdź pełny tekst źródłaMiles, Richard B. Filtered Rayleigh scattering measurements in supersonic/hypersonic facilities. Washington: AIAA, 1992.
Znajdź pełny tekst źródłaCenter, Langley Research, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.
Znajdź pełny tekst źródłaD, Carboni Jeanne, Supersonic investigation of two dimensional .... i United States. National Aeronautics and Space Administration., red. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.
Znajdź pełny tekst źródłaD, Carboni Jeanne, Supersonic investigation of two dimensional... i United States. National Aeronautics and Space Administration., red. Supersonic investigation of two-dimensional hypersonic exhaust nozzles. [Washington, DC: National Aeronautics and Space Administration, 1992.
Znajdź pełny tekst źródłaL, Pittman Jimmy, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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.
Znajdź pełny tekst źródłaCzęści książek na temat "Supersonic / hypersonic"
Ingenito, Antonella. "Design of Supersonic/Hypersonic Vehicles". W Subsonic Combustion Ramjet Design, 9–17. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-66881-5_3.
Pełny tekst źródłaStemmer, Christian, i Nikolaus A. Adams. "Supersonic and Hypersonic Boundary-Layer Flows". W 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.
Pełny tekst źródłaVervisch, P., i A. Bourdon. "The Recombination of Ionized Species in Supersonic Flows". W Molecular Physics and Hypersonic Flows, 525–42. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-0267-1_35.
Pełny tekst źródłaMarcos, T. V. C., D. Romanelli Pinto, G. S. Moura, A. C. Oliveira, J. B. Chanes, P. G. P. Toro i M. A. S. Minucci. "Supersonic Combustion Flow Visualization at Hypersonic Flow". W 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.
Pełny tekst źródłaWegener, Peter P. "Toward High Speed: Supersonic and Hypersonic Flight". W What Makes Airplanes Fly?, 145–66. New York, NY: Springer US, 1991. http://dx.doi.org/10.1007/978-1-4684-0403-6_10.
Pełny tekst źródłaWegener, Peter P. "Toward High Speed: Supersonic and Hypersonic Flight". W 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.
Pełny tekst źródłaSmits, Alexander J., i M. Pino Martin. "Turbulence in Supersonic and Hypersonic Boundary Layers". W Solid mechanics and its applications, 221–30. Dordrecht: Springer Netherlands, 2006. http://dx.doi.org/10.1007/978-1-4020-4150-1_21.
Pełny tekst źródłaVerhoff, A., D. C. Stookesberry, B. M. Hopping i T. R. Michal. "Supersonic/Hypersonic Euler Flowfield Prediction Method for Aircraft Configurations". W 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.
Pełny tekst źródłaRomanelli Pinto, D., T. V. C. Marcos, R. L. M. Alcaide, A. C. Oliveira, J. B. Chanes, P. G. P. Toro i M. A. S. Minucci. "Supersonic Combustion Experimental Investigation at T2 Hypersonic Shock Tunnel". W 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.
Pełny tekst źródłaSeror, S., i L. Kosarev. "Turbulence Compressibility Effects for Supersonic and Hypersonic Separated Flows". W 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.
Pełny tekst źródłaStreszczenia konferencji na temat "Supersonic / hypersonic"
MASON, W., i JAEWOO LEE. "On optimal supersonic/hypersonic bodies". W Flight Simulation Technologies Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-3072.
Pełny tekst źródłaSOBIECZKY, H. "Generic supersonic and hypersonic configurations". W 9th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3301.
Pełny tekst źródłaYOON, W., i T. CHUNG. "Numerical studies of supersonic/hypersonic combustion". W 30th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-94.
Pełny tekst źródłaLandon, Mark, Darryl Hall, Jerry Udy i Ernest Perry. "Automatic supersonic/hypersonic aerodynamic shape optimization". W 12th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-1898.
Pełny tekst źródłaAbouali, Omid, i Goodarz Ahmadi. "Bow Shock Effect on Particle Transport and Deposition in a Hypersonic Impactor". W ASME/JSME 2003 4th Joint Fluids Summer Engineering Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/fedsm2003-45072.
Pełny tekst źródłaZhang, Chen-an, Zheng-yin Ye i Wei-wei Zhang. "Aeroservoelastic Analysis for Supersonic and Hypersonic Missiles". W 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.
Pełny tekst źródłaNICKERSON, G., S. DUNN i D. MIGDAL. "Optimized supersonic exhaust nozzles for hypersonic propulsion". W 24th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3161.
Pełny tekst źródłaArai, Takakage, Sosuke Sugano i Shoji Sakaue. "Interaction between Supersonic Cavity Flow and Streamwise Vortices for Supersonic Mixing Enhancement". W 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.
Pełny tekst źródłaThakur, Amit, i Corin Segal. "Flameholding Analyses in Supersonic Flow". W 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.
Pełny tekst źródłaAbouali, Omid, i Goodarz Ahmadi. "Numerical Modeling of Upstream Nozzle Effect in Supersonic/Hypersonic Impactors for Nano-Particles". W ASME 2005 Fluids Engineering Division Summer Meeting. ASMEDC, 2005. http://dx.doi.org/10.1115/fedsm2005-77433.
Pełny tekst źródłaRaporty organizacyjne na temat "Supersonic / hypersonic"
Kostoff, Ronald N., Henry J. Eberhart i Darrell R. Toothman. Science and Technology Text Mining: Hypersonic and Supersonic Flow. Fort Belvoir, VA: Defense Technical Information Center, listopad 2003. http://dx.doi.org/10.21236/ada418717.
Pełny tekst źródłaHerbert, Thorwald. Stability of Boundary Layers at High Supersonic and Hypersonic Speeds. Fort Belvoir, VA: Defense Technical Information Center, maj 1992. http://dx.doi.org/10.21236/ada250900.
Pełny tekst źródłaLempert, Walter R., i Richard B. Miles. Quantitative Imaging of Time-Evolving Structure for Supersonic and Hypersonic Flows. Fort Belvoir, VA: Defense Technical Information Center, marzec 1995. http://dx.doi.org/10.21236/ada297721.
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