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Статті в журналах з теми "Hypersonic boundary-layer transition"
Berry, Scott A., Thomas J. Horvath, Brian R. Hollis, Rick A. Thompson, and H. Harris Hamilton. "X-33 Hypersonic Boundary-Layer Transition." Journal of Spacecraft and Rockets 38, no. 5 (September 2001): 646–57. http://dx.doi.org/10.2514/2.3750.
Повний текст джерелаMATSUYAMA, Shingo. "DNS of Hypersonic Boundary Layer Transition." Journal of the Visualization Society of Japan 41, no. 162 (2021): 13–14. http://dx.doi.org/10.3154/jvs.41.162_13.
Повний текст джерелаZhao, Yatian, Zhiyuan Shao, and Hongkang Liu. "Aerodisk Effect on Hypersonic Boundary Layer Transition and Heat Transfer of HIFiRE-5 Vehicle." Aerospace 9, no. 12 (November 23, 2022): 742. http://dx.doi.org/10.3390/aerospace9120742.
Повний текст джерелаKimmel, Roger L. "Introduction: Roughness and Hypersonic Boundary-Layer Transition." Journal of Spacecraft and Rockets 45, no. 6 (November 2008): 1089. http://dx.doi.org/10.2514/1.41332.
Повний текст джерелаKuntz, David W., and Donald L. Potter. "Boundary-Layer Transition and Hypersonic Flight Testing." Journal of Spacecraft and Rockets 45, no. 2 (March 2008): 184–92. http://dx.doi.org/10.2514/1.29708.
Повний текст джерелаTONG, FuLin, JianQiang CHEN, GuoHua TU, GuoLiang XU, JiuFen CHEN, BingBing WAN, XianXu YUAN, and YiFeng ZHANG. "Recent progresses on hypersonic boundary-layer transition." SCIENTIA SINICA Physica, Mechanica & Astronomica 49, no. 11 (May 1, 2019): 114701. http://dx.doi.org/10.1360/sspma-2019-0071.
Повний текст джерелаPatrick, Chris. "Total temperature affects hypersonic boundary layer transition." Scilight 2019, no. 47 (November 22, 2019): 471107. http://dx.doi.org/10.1063/10.0000281.
Повний текст джерелаDong, Hao, Shicheng Liu, Xi Geng, and Keming Cheng. "Study on Oil-Film Interferometry Measurement Technique of Hypersonic Boundary Layer Transition." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 36, no. 6 (December 2018): 1156–61. http://dx.doi.org/10.1051/jnwpu/20183661156.
Повний текст джерелаLiu, Meikuan, Guilai Han, Zongxian Li, and Zonglin Jiang. "Experimental study on the effects of the cone nose-tip bluntness." Physics of Fluids 34, no. 10 (October 2022): 101703. http://dx.doi.org/10.1063/5.0110928.
Повний текст джерелаLee, Cunbiao, and Shiyi Chen. "Recent progress in the study of transition in the hypersonic boundary layer." National Science Review 6, no. 1 (May 7, 2018): 155–70. http://dx.doi.org/10.1093/nsr/nwy052.
Повний текст джерелаДисертації з теми "Hypersonic boundary-layer transition"
Atcliffe, Phillip Arthur. "Effects of boundary layer separation and transition at hypersonic speeds." Thesis, Cranfield University, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.336458.
Повний текст джерелаRiley, Zachary Bryce Riley. "Interaction Between Aerothermally Compliant Structures and Boundary-Layer Transition in Hypersonic Flow." The Ohio State University, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=osu1471618528.
Повний текст джерелаHusmeier, Frank. "Numerical Investigations of Transition in Hypersonic Flows over Circular Cones." Diss., The University of Arizona, 2008. http://hdl.handle.net/10150/196123.
Повний текст джерелаTirtey, Sandy C. "Characterization of a transitional hypersonic boundary layer in wind tunnel and flight conditions." Doctoral thesis, Universite Libre de Bruxelles, 2009. http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/210367.
Повний текст джерелаA wide bibliographic review describing the main parameters affecting transition and their coupling is proposed. The most popular roughness-induced transition predictions correlations are presented, insisting on the lack of physics included in these methods and the difficulties encountered in performing ground hypersonic transition experiments representative of real flight characteristics. This bibliographic review shows the importance of a better understanding of the physical phenomenon and of a wider experimental database, including real flight data, for the development of accurate prediction methods.
Based on the above conclusions, a hypersonic experimental test campaign is realized for the characterization of the flow field structure in the vicinity and in the wake of 3D roughness elements. This fundamental flat plate study is associated with numerical simulations for supporting the interpretation of experimental results and thus a better understanding of transition physics. Finally, a model is proposed in agreement with the wind tunnel observations and the bibliographic survey.
The second principal axis of the present study is the development of a hypersonic in-flight roughness-induced transition experiment in the frame of the European EXPERT program. These flight data, together with various wind tunnel measurements are very important for the development of a wide experimental database supporting the elaboration of future transition prediction methods.
Doctorat en Sciences de l'ingénieur
info:eu-repo/semantics/nonPublished
Laible, Andreas Christian. "Numerical Investigation of Boundary-Layer Transition for Cones at Mach 3.5 and 6.0." Diss., The University of Arizona, 2011. http://hdl.handle.net/10150/205419.
Повний текст джерелаGrossir, Guillaume. "Longshot hypersonic wind tunnel flow characterization and boundary layer stability investigations." Doctoral thesis, Universite Libre de Bruxelles, 2015. http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/209044.
Повний текст джерелаEmphasis is initially placed on the flow characterization of the Longshot wind tunnel where these experiments are performed. Free-stream static pressure diagnostics are implemented in order to complete existing stagnation point pressure and heat flux measurements on a hemispherical probe. An alternative method used to determine accurate free-stream flow conditions is then derived following a rigorous theoretical approach coupled to the VKI Mutation thermo-chemical library. Resulting sensitivities of free-stream quantities to the experimental inputs are determined and the corresponding uncertainties are quantified and discussed. The benefits of this different approach are underlined, revealing the severe weaknesses of traditional methods based on the measurement of reservoir conditions and the following assumptions of an isentropic and adiabatic flow through the nozzle. The operational map of the Longshot wind tunnel is redefined accordingly. The practical limits associated with the onset of nitrogen flow condensation under non-equilibrium conditions are also accounted for.
Boundary layer transition experiments are then performed in this environment with free-stream Mach numbers ranging between 10-12. Instrumentation along the 800mm long conical model includes flush-mounted thermocouples and fast-response pressure sensors. Transition locations on sharp cones compare favorably with engineering correlations. A strong stabilizing effect of nosetip bluntness is reported and no transition reversal regime is observed for Re_RN<120000. Wavelet analysis of wall pressure traces denote the presence of inviscid instabilities belonging to Mack's second mode. An excellent agreement with Linear Stability Theory results is obtained from which the N-factor of the Longshot wind tunnel in these conditions is inferred. A novel Schlieren technique using a short duration laser light source is developed, allowing for high-quality flow visualization of the boundary layer disturbances. Comparisons of these measurement techniques between each other are finally reported, providing a detailed view of the transition process above Mach 10.
Doctorat en Sciences de l'ingénieur
info:eu-repo/semantics/nonPublished
Sivasubramanian, Jayahar. "Numerical Investigation of Laminar-Turbulent Transition in a Cone Boundary Layer at Mach 6." Diss., The University of Arizona, 2012. http://hdl.handle.net/10150/228514.
Повний текст джерелаYentsch, Robert J. "Three-Dimensional Shock-Boundary Layer Interactions in Simulations of HIFiRE-1 and HIFiRE-2." The Ohio State University, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=osu1384195671.
Повний текст джерелаPadilla, Montero Ivan. "Analysis of the stability of a flat-plate high-speed boundary layer with discrete roughness." Doctoral thesis, Universite Libre de Bruxelles, 2021. https://dipot.ulb.ac.be/dspace/bitstream/2013/324490/5/contratPM.pdf.
Повний текст джерелаDoctorat en Sciences de l'ingénieur et technologie
info:eu-repo/semantics/nonPublished
Di, Giovanni Antonio [Verfasser], Christian [Akademischer Betreuer] Stemmer, Wolfgang [Gutachter] Schröder, and Christian [Gutachter] Stemmer. "Roughness-Induced Transition in a Hypersonic Capsule Boundary Layer under Wind-Tunnel and Reentry Conditions / Antonio Di Giovanni ; Gutachter: Wolfgang Schröder, Christian Stemmer ; Betreuer: Christian Stemmer." München : Universitätsbibliothek der TU München, 2020. http://d-nb.info/1211725227/34.
Повний текст джерелаКниги з теми "Hypersonic boundary-layer transition"
Wendt, Volker. Experimentelle Untersuchung der Instabilitat von ebenen und konischen laminaren Hyperschallgrenzschichten. Koln, Germany: DLR, 1993.
Знайти повний текст джерелаRichards, W. Lance. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.
Знайти повний текст джерелаThree-Dimensional Hypersonic Boundary Layer Stability and Transition. Storming Media, 1997.
Знайти повний текст джерелаA, Thompson R., and United States. National Aeronautics and Space Administration., eds. Hypersonic boundary-layer transition for X-33 phase II vehicle. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.
Знайти повний текст джерелаA, Thompson R., and United States. National Aeronautics and Space Administration., eds. Hypersonic boundary-layer transition for X-33 phase II vehicle. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.
Знайти повний текст джерелаA, Thompson R., and United States. National Aeronautics and Space Administration., eds. Hypersonic boundary-layer transition for X-33 phase II vehicle. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.
Знайти повний текст джерелаA, Thompson R., and United States. National Aeronautics and Space Administration., eds. Hypersonic boundary-layer transition for X-33 phase II vehicle. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.
Знайти повний текст джерелаThermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.
Знайти повний текст джерелаThermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.
Знайти повний текст джерелаA quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone: Final report. Norfolk, Va: Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University, 1996.
Знайти повний текст джерелаЧастини книг з теми "Hypersonic boundary-layer transition"
Stetson, Kenneth F. "Hypersonic Boundary-Layer Transition." In Advances in Hypersonics, 324–417. Boston, MA: Birkhäuser Boston, 1992. http://dx.doi.org/10.1007/978-1-4612-0379-7_7.
Повний текст джерелаMalik, M. R. "Hypersonic Boundary-Layer Receptivity and Stability." In Laminar-Turbulent Transition, 409–14. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-03997-7_61.
Повний текст джерелаMaslov, A. A., T. Poplavskaya, and D. A. Bountin. "Hypersonic boundary layer transition and control." In Seventh IUTAM Symposium on Laminar-Turbulent Transition, 19–26. Dordrecht: Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-3723-7_3.
Повний текст джерелаMaslov, A. A., and S. G. Mironov. "Experimental Investigations of the Hypersonic Boundary Layer Stability." In Laminar-Turbulent Transition, 421–26. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-03997-7_63.
Повний текст джерелаFu, S., and L. Wang. "Modeling Flow Transition in Hypersonic Boundary Layer." In New Trends in Fluid Mechanics Research, 53–56. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-75995-9_9.
Повний текст джерелаMorozov, S. O., S. V. Lukashevich, and A. N. Shiplyuk. "Hypersonic Boundary Layer Instability and Control by Passive Porous Coatings." In IUTAM Laminar-Turbulent Transition, 613–19. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-67902-6_53.
Повний текст джерелаSidharth, G. S., A. Dwivedi, J. W. Nichols, M. Jovanović, and G. V. Candler. "Global Linear Stability and Sensitivity of Hypersonic Shock-Boundary Layer Interactions." In IUTAM Laminar-Turbulent Transition, 489–98. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-67902-6_42.
Повний текст джерелаGroskopf, Gordon, and Markus J. Kloker. "Effects of an Oblique Roughness on Hypersonic Boundary-Layer Transition." In High Performance Computing in Science and Engineering ‘12, 255–76. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-33374-3_20.
Повний текст джерелаYu, Min, Wu-bing Yang, and Xiang-jiang Yuan. "Numerical Study of Görtler Vortices on Hypersonic Boundary-Layer Transition." In Lecture Notes in Electrical Engineering, 416–22. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_33.
Повний текст джерелаXie, S. F., F. Ji, D. Yao, and Q. Shen. "Experimental Study of Hypersonic Shock Wave/Transition Boundary Layer Interaction." In 31st International Symposium on Shock Waves 1, 1015–24. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91020-8_122.
Повний текст джерелаТези доповідей конференцій з теми "Hypersonic boundary-layer transition"
Berry, Scott, Thomas Horvath, Brian Hollis, H. Hamilton, II, and Richard Thompson. "X-33 hypersonic boundary layer transition." In 33rd Thermophysics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-3560.
Повний текст джерелаMALIK, M., T. ZANG, and D. BUSHNELL. "Boundary layer transition in hypersonic flows." In 2nd International Aerospace Planes Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-5232.
Повний текст джерелаKuntz, David, and Donald Potter. "Boundary Layer Transition and Hypersonic Flight Testing." In 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-308.
Повний текст джерелаKimmel, Roger. "Aspects of Hypersonic Boundary Layer Transition Control." In 41st Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-772.
Повний текст джерелаShrestha, Prakash, Joseph W. Nichols, Mihailo R. Jovanovic, and Graham V. Candler. "Study of Trip-Induced Hypersonic Boundary Layer Transition." In 47th AIAA Fluid Dynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4513.
Повний текст джерелаSchneider, Steven. "Effects of Roughness on Hypersonic Boundary-Layer Transition." In 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-305.
Повний текст джерелаJohnson, Heath, and Graham Candler. "PSE analysis of reacting hypersonic boundary layer transition." In 30th Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-3793.
Повний текст джерелаSchneider, Steven. "Hypersonic Boundary-Layer Transition with Ablation and Blowing." In 38th Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-3730.
Повний текст джерелаBerry, Scott, Roger Kimmel, and Eli Reshotko. "Recommendations for Hypersonic Boundary Layer Transition Flight Testing." In 41st AIAA Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-3415.
Повний текст джерелаRiley, Zachary, Rohit Deshmukh, Brent A. Miller, and Jack J. McNamara. "Characterization of Structural Response to Hypersonic Boundary Layer Transition." In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-0688.
Повний текст джерелаЗвіти організацій з теми "Hypersonic boundary-layer transition"
Stetson, Kenneth F. Comments on Hypersonic Boundary-Layer Transition. Fort Belvoir, VA: Defense Technical Information Center, September 1990. http://dx.doi.org/10.21236/ada227242.
Повний текст джерелаKimmel, Roger L., and J. Poggie. Three-Dimensional Hypersonic Boundary Layer Stability and Transition. Fort Belvoir, VA: Defense Technical Information Center, December 1997. http://dx.doi.org/10.21236/ada417303.
Повний текст джерелаMaslov, Anatoly A. Experimental Study of Stability and Transition of Hypersonic Boundary Layer Around Blunted Cone. Fort Belvoir, VA: Defense Technical Information Center, December 2001. http://dx.doi.org/10.21236/ada408241.
Повний текст джерелаSchneider, Steven P. Hypersonic Boundary-Layer Transition Research in the Boeing/AFOSR Mach-6 Quiet Tunnel. Fort Belvoir, VA: Defense Technical Information Center, March 2006. http://dx.doi.org/10.21236/ada448081.
Повний текст джерелаZhong, Xiaolin. Numerical Simulation of Hypersonic Boundary Layer Receptivity, Transient Growth and Transition With Surface Roughness. Fort Belvoir, VA: Defense Technical Information Center, December 2009. http://dx.doi.org/10.21236/ada517055.
Повний текст джерелаAeschliman, D. P., R. H. Croll, and D. W. Kuntz. Use of shear-stress-sensitive, temperature-insensitive liquid crystals for hypersonic boundary-layer transition detection. Office of Scientific and Technical Information (OSTI), April 1997. http://dx.doi.org/10.2172/469193.
Повний текст джерелаGrossir, Guillaume. On the design of quiet hypersonic wind tunnels. Von Karman Institute for Fluid Dynamics, December 2020. http://dx.doi.org/10.35294/tm57.
Повний текст джерелаKimmel, Roger, David Adamczak, Ryan Gosse, Karen Berger, and Shann Rufer. Ground Test and Computation of Boundary Layer Transition on the Hypersonic International Flight Research and Experimentation (HIFiRE)-5 Vehicle. Fort Belvoir, VA: Defense Technical Information Center, February 2011. http://dx.doi.org/10.21236/ada548272.
Повний текст джерелаStetson, Kenneth F. Hypersonic Laminar Boundary Layer Transition. Part 1. Nosetip Bluntness Effects on Cone Frustum Transition. Part 2. Mach 6 Experiments of Transition on a Cone at Angle of Attack. Fort Belvoir, VA: Defense Technical Information Center, December 1986. http://dx.doi.org/10.21236/ada178877.
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