Добірка наукової літератури з теми "Experimental Hypersonic flow"
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Статті в журналах з теми "Experimental Hypersonic flow"
GROENIG, Hans, and Herbert OLIVER. "Experimental Hypersonic Flow Research in Europe." JSME International Journal Series B 41, no. 2 (1998): 397–407. http://dx.doi.org/10.1299/jsmeb.41.397.
Повний текст джерелаFan, Xiaoqiang, and Yuan Tao. "Investigation of Flow Control for the Hypersonic Inlets via Counter Flow." International Journal of Aerospace Engineering 2015 (2015): 1–8. http://dx.doi.org/10.1155/2015/956317.
Повний текст джерелаKalimuthu, R., R. C. Mehta, and E. Rathakrishnan. "Experimental investigation on spiked body in hypersonic flow." Aeronautical Journal 112, no. 1136 (October 2008): 593–98. http://dx.doi.org/10.1017/s0001924000002554.
Повний текст джерелаPapuccuoglu, Hakan. "Experimental investigation of hypersonic three-dimensional corner flow." AIAA Journal 31, no. 4 (April 1993): 652–56. http://dx.doi.org/10.2514/3.11599.
Повний текст джерелаLaitón, Sergio Nicolas Pachón, João Felipe de Araujo Martos, Israel da Silveira Rego, George Santos Marinho, and Paulo Gilberto de Paula Toro. "Experimental Study of Single Expansion Ramp Nozzle Performance Using Pitot Pressure and Static Pressure Measurements." International Journal of Aerospace Engineering 2019 (February 27, 2019): 1–11. http://dx.doi.org/10.1155/2019/7478129.
Повний текст джерелаJuluru Sandeep and AVSS Kumara Swami Gupta. "Grid Adaptive Technique for Simulation of Scramjet Intake-Isolator at Hypersonic Speeds." Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 101, no. 1 (January 18, 2023): 73–89. http://dx.doi.org/10.37934/arfmts.101.1.7389.
Повний текст джерелаLanson, F., and J. L. Stollery. "Some hypersonic intake studies." Aeronautical Journal 110, no. 1105 (March 2006): 145–56. http://dx.doi.org/10.1017/s0001924000001123.
Повний текст джерелаV. Gromyko, Yuriy, Anatoliy A. Maslov, Andrey A. Sidorenko, Pavel A. Polivanov, and Ivan S. Tsyryulnikov. "Estimation of the Flow Parametrs in Hypersonic Wind Tunnels." Siberian Journal of Physics 6, no. 2 (July 1, 2011): 10–16. http://dx.doi.org/10.54362/1818-7919-2011-6-2-10-16.
Повний текст джерелаCreighton, S., and R. Hillier. "Experimental and computational study of unsteady hypersonic cavity flows." Aeronautical Journal 111, no. 1125 (November 2007): 673–88. http://dx.doi.org/10.1017/s0001924000004851.
Повний текст джерелаDONG, HAO, CHENG-PENG WANG, and KE-MING CHENG. "EXPERIMENTAL AND NUMERICAL INVESTIGATION OF HYPERSONIC JAWS INLET." Modern Physics Letters B 24, no. 13 (May 30, 2010): 1409–12. http://dx.doi.org/10.1142/s0217984910023748.
Повний текст джерелаДисертації з теми "Experimental Hypersonic flow"
Mohammed, Sohail. "Experimental investigation of shock wave and boundary layer interaction near convex corners in hypersonic flow." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp01/MQ28817.pdf.
Повний текст джерелаSaad, Mohd Rashdan. "Experimental studies on shock boundary layer interactions using micro-ramps at Mach 5." Thesis, University of Manchester, 2013. https://www.research.manchester.ac.uk/portal/en/theses/experimental-studies-on-shock-boundary-layer-interactions-using-microramps-at-mach-5(71f1e11c-dbfd-443a-a9ee-e3fc160176f1).html.
Повний текст джерелаBoyd, Robert Raymond. "An Experimental and Computational Investigation on the Effect of Transonic Flow in Hypersonic Wind Tunnel Nozzles, Including Filtered Rayleigh Scattering Measurements /." The Ohio State University, 1996. http://rave.ohiolink.edu/etdc/view?acc_num=osu148793364864785.
Повний текст джерелаChpoun, Amer. "Contribution a l'etude d'ecoulements hypersoniques (m=5) sur une rampe de compression en configuration 2-d et 3-d." Paris 6, 1988. http://www.theses.fr/1988PA06A005.
Повний текст джерелаChpoun, Amer. "Contribution à l'étude d'écoulements hypersoniques (M=5) sur une rampe de compression en configuration 2-D et 3-D." Paris 6, 1988. http://www.theses.fr/1988PA066149.
Повний текст джерелаDenman, Paul Ashley. "Experimental study of hypersonic boundary layers and base flows." Thesis, Imperial College London, 1996. http://hdl.handle.net/10044/1/45466.
Повний текст джерелаNieberding, Zachary J. "An Investigation of Acoustic Wave Propagation in Mach 2 Flow." University of Cincinnati / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881591.
Повний текст джерелаO'Dowd, Devin Owen. "Aero-thermal performance of transonic high-pressure turbine blade tips." Thesis, University of Oxford, 2010. http://ora.ox.ac.uk/objects/uuid:e7b8e7d0-4973-4757-b4df-415723e7562f.
Повний текст джерелаNagashetty, K. "Experimental Investigations on Hypersonic Waverider." Thesis, 2014. http://hdl.handle.net/2005/3195.
Повний текст джерелаKumar, Chintoo Sudhiesh. "Experimental Investigation Of Aerodynamic Interference Heating Due To Protuberances On Flat Plates And Cones Facing Hypersonic Flows." Thesis, 2013. http://etd.iisc.ernet.in/handle/2005/2621.
Повний текст джерелаКниги з теми "Experimental Hypersonic flow"
R, Keener Earl, Hui Frank C. L, and Ames Research Center, eds. Experimental results for a hypersonic nozzle/afterbody flow field. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.
Знайти повний текст джерелаHughson, M. C. Hypersonic prediction comparisons with experimental data for a cone-cylinder at Mach 6.86. Eglin Air Force Base, Fl: Air Force Armament Laboratory, Eglin Air Force Base, 1989.
Знайти повний текст джерелаW, Paulson John, Weilmuenster K. James, and United States. National Aeronautics and Space Administration., eds. Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.
Знайти повний текст джерелаNagamatsu, Henry T. Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.
Знайти повний текст джерелаCenter, Langley Research, ed. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаHolland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Experimental aerothermodynamic research of hypersonic aircraft: Technical progress report (substitution) for the period October 1, 1988 - March 31, 1989. [Washington, DC: National Aeronautics and Space Administration, 1989.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Experimental aerothermodynamic research of hypersonic aircraft: Technical progress report (substitution) for the period March 1, 1987 - September 30, 1987. [Washington, DC: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаAvery, Don E. Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Знайти повний текст джерелаWells, William L. Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air. Hampton, Va: Langley Research Center, 1990.
Знайти повний текст джерелаЧастини книг з теми "Experimental Hypersonic flow"
Henckels, A., and F. Maurer. "Hypersonic Corner Flow Detailed Experimental Study." In Hypersonic Flows for Reentry Problems, 441–54. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-77922-0_41.
Повний текст джерелаVetter, M., H. Olivier, and H. Grönig. "Flow over double ellipsoid and sphere — Experimental results." In Hypersonic Flows for Reentry Problems, 489–500. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-77922-0_45.
Повний текст джерелаChazot, Olivier. "Aerospace Flight Modeling and Experimental Testing." In Uncertainty in Engineering, 131–47. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-83640-5_9.
Повний текст джерелаAupoix, B. "Experimental Validation of Hypersonic Viscous Flow Models." In New Trends in Instrumentation for Hypersonic Research, 41–50. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-011-1828-6_4.
Повний текст джерелаAymer, D., T. Alziary, L. De Luca, and G. Carlomagno. "Experimental Study of the Flow Around a Double Ellipsoid Configuration." In Hypersonic Flows for Reentry Problems, 335–57. Berlin, Heidelberg: Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-76527-8_27.
Повний текст джерелаLinde, Magnus. "Leeside Flow over Delta Wing at M = 7.15 Experimental results for Test Case 7.1.2." In Hypersonic Flows for Reentry Problems, 927–32. Berlin, Heidelberg: Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-76527-8_60.
Повний текст джерелаHavermann, M., and F. Seiler. "Boundary Layer Influence on Supersonic Jet/Cross-Flow Interaction in Hypersonic Flow." In New Results in Numerical and Experimental Fluid Mechanics V, 281–88. Berlin, Heidelberg: Springer Berlin Heidelberg, 2006. http://dx.doi.org/10.1007/978-3-540-33287-9_35.
Повний текст джерелаHenckels, A., and F. Maurer. "Experimental Study of the Longitudinal Hypersonic Corner Flow Field Hermes-R&D Research Program, Problem No. 5." In Hypersonic Flows for Reentry Problems, 315–31. Berlin, Heidelberg: Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-76527-8_26.
Повний текст джерелаSchrijer, F. F. J., R. Caljouw, F. Scarano, and B. W. van Oudheusden. "Three dimensional experimental investigation of a hypersonic double-ramp flow." In Shock Waves, 719–24. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-85168-4_116.
Повний текст джерелаRolim, T. C., and F. K. Lu. "Experimental Investigation of a Hypersonic Inlet with Variable Sidewall for Flow Control." In 29th International Symposium on Shock Waves 2, 1003–8. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-16838-8_33.
Повний текст джерелаТези доповідей конференцій з теми "Experimental Hypersonic flow"
Hutchins, Kelley, Maruthi Akella, Noel Clemens, and Jeffrey Donbar. "Detection and Transient Dynamics Modeling of Experimental Hypersonic Inlet Unstart." In 6th AIAA Flow Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-2808.
Повний текст джерелаLi, Suxun, Yongkang Chen, Yulin Li, Suxun Li, Yongkang Chen, and Yulin Li. "Hypersonic flow over double-ellipsoid - Experimental investigation." In 15th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-2287.
Повний текст джерелаBez, Jean-Pierre, Jean-Jacques Chattot, and Francois Noel. "Some Validations by Experimental Results in Hypersonic Flow Computations." In Aerospace Vehicle Conference. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1988. http://dx.doi.org/10.4271/880925.
Повний текст джерелаde Luca, Luigi, and Gennaro Cardone. "Experimental analysis of Goertler vortices in hypersonic wedge flow." In Aerospace Sensing, edited by Jan K. Eklund. SPIE, 1992. http://dx.doi.org/10.1117/12.58544.
Повний текст джерелаSPAID, FRANK, and EARL KEENER. "Experimental results for a hypersonic nozzle/afterbody flow field." In 28th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3915.
Повний текст джерелаSingh, Amarjit, and J. Stollery. "Experimental investigation of hypersonic flow over a wing-body combination." In International Aerospace Planes and Hypersonics Technologies. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-6083.
Повний текст джерелаEngblom, W., B. Yuceil, D. Goldstein, and D. Dolling. "Hypersonic forward-facing cavity flow - An experimental and numerical study." In 33rd Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-293.
Повний текст джерелаKaga, T., T. Matsu-Ura, and T. Fujiwara. "Experimental study of ablation gas jet opposing to hypersonic flow." In 40th AIAA Aerospace Sciences Meeting & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-297.
Повний текст джерелаKarpuzcu, Irmak Taylan, Deborah A. Levin, Derek Mamrol, Lauren N. Wagner, Mark E. Noftz, Joseph S. Jewell, and Sonya T. Smith. "Jet Flow - Shockwave Interactions in a Hypersonic Flow using Experimental and Kinetic Methods." In AIAA SCITECH 2022 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-1577.
Повний текст джерелаZhongjie, Shao, Xing Chen, Dan Wang, and Wang Yuan. "Experimental study of hypersonic boundary layer flow control based on isolated roughness." In THE 6th NTERNATIONAL CONFERENCE ON FLUID FLOW, HEAT AND MASS TRANSFER. Avestia Publishing, 2019. http://dx.doi.org/10.11159/ffhmt19.153.
Повний текст джерелаЗвіти організацій з теми "Experimental Hypersonic flow"
Schneider, Steven P. Completion of the 9.5-Inch Mach-6 Ludwieg Tube: Enabling Low-Cost Hypersonic Quiet-Flow Experiments. Fort Belvoir, VA: Defense Technical Information Center, February 2001. http://dx.doi.org/10.21236/ada387557.
Повний текст джерела