Добірка наукової літератури з теми "Quiet Tunnels"
Оформте джерело за APA, MLA, Chicago, Harvard та іншими стилями
Ознайомтеся зі списками актуальних статей, книг, дисертацій, тез та інших наукових джерел на тему "Quiet Tunnels".
Біля кожної праці в переліку літератури доступна кнопка «Додати до бібліографії». Скористайтеся нею – і ми автоматично оформимо бібліографічне посилання на обрану працю в потрібному вам стилі цитування: APA, MLA, «Гарвард», «Чикаго», «Ванкувер» тощо.
Також ви можете завантажити повний текст наукової публікації у форматі «.pdf» та прочитати онлайн анотацію до роботи, якщо відповідні параметри наявні в метаданих.
Статті в журналах з теми "Quiet Tunnels"
Schneider, Steven P. "Development of Hypersonic Quiet Tunnels." Journal of Spacecraft and Rockets 45, no. 4 (July 2008): 641–64. http://dx.doi.org/10.2514/1.34489.
Повний текст джерелаLiang, Zhengzhao, Xiangxin Liu, Yanbo Zhang, and Chunan Tang. "Analysis of Precursors Prior to Rock Burst in Granite Tunnel Using Acoustic Emission and Far Infrared Monitoring." Mathematical Problems in Engineering 2013 (2013): 1–10. http://dx.doi.org/10.1155/2013/214340.
Повний текст джерелаQuinn, Daniel B., Anthony Watts, Tony Nagle, and David Lentink. "A new low-turbulence wind tunnel for animal and small vehicle flight experiments." Royal Society Open Science 4, no. 3 (March 2017): 160960. http://dx.doi.org/10.1098/rsos.160960.
Повний текст джерелаSchneider, Steven P. "Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels." Progress in Aerospace Sciences 72 (January 2015): 17–29. http://dx.doi.org/10.1016/j.paerosci.2014.09.008.
Повний текст джерелаGhoreyshi, M., A. D. H. Kim, A. Jirasek, A. J. Lofthouse, and R. M. Cummings. "Validation of CFD simulations for X-31 wind-tunnel models." Aeronautical Journal 119, no. 1214 (April 2015): 479–500. http://dx.doi.org/10.1017/s0001924000010575.
Повний текст джерелаHasan, Mohammed Munif, and Shabudin Mat. "Data Reduction Analysis on UTM-LST External Balance." International Journal for Research in Applied Science and Engineering Technology 10, no. 10 (October 31, 2022): 952–59. http://dx.doi.org/10.22214/ijraset.2022.47097.
Повний текст джерелаLiu, Tong, Yujian Zhong, Zhihua Feng, Wei Xu, Feiting Song, and Chenghan Li. "New Construction Technology of a Shallow Tunnel in Boulder-Cobble Mixed Grounds." Advances in Civil Engineering 2020 (March 21, 2020): 1–20. http://dx.doi.org/10.1155/2020/5686042.
Повний текст джерелаDuan, Xu, Qi Dong, and Wanjun Ye. "Experimental Study on Seismic Performance of Prefabricated Utility Tunnel." Advances in Civil Engineering 2019 (October 27, 2019): 1–14. http://dx.doi.org/10.1155/2019/8968260.
Повний текст джерелаKhan, Babar, Syed Muhammad Jamil, Jung Joo Kim, Turab H. Jafri, and Jonguk Kim. "Rock Mass Behavior under Tunnel Widening in Asymmetric and Symmetric Modes Considering Different Shapes and Parametric Conditions." Geosciences 9, no. 12 (December 16, 2019): 518. http://dx.doi.org/10.3390/geosciences9120518.
Повний текст джерелаBlanchard, Alan E., Jason T. Lachowicz, and Stephen P. Wilkinson. "NASA Langley Mach 6 Quiet Wind-Tunnel Performance." AIAA Journal 35, no. 1 (January 1997): 23–28. http://dx.doi.org/10.2514/2.82.
Повний текст джерелаДисертації з теми "Quiet Tunnels"
Manning, Melissa Lynn. "COMPUTATIONAL EVALUATION OF QUIET TUNNEL HYPERSONIC BOUNDARY LAYER STABILITY EXPERIMENTS." NCSU, 2001. http://www.lib.ncsu.edu/theses/available/etd-20010112-081130.
Повний текст джерелаManning, Melissa Lynn. Computational Evaluation of Quiet Tunnel Hypersonic Boundary Layer Stability Experiments. (Under the direction of Dr. Ndaona Chokani.) A computational evaluation of two stability experiments conducted in the NASA Langley Mach 6 axisymmetric quiet nozzle test chamber facility is conducted. Navier-Stokes analysis of the mean flow and linear stability theory analysis of boundary layer disturbances is performed in the computations. The effects of adverse pressure gradient and wall cooling are examined. Calculated pressure, temperature and boundary layer thickness distributions show very good overall agreement with experimental measurements. Computed mass flux and total temperature profiles show very good quantitative agreement with uncalibrated hot-wire measurements obtained with the hot-wire operated in high and low overheat modes respectively. Comparisons between calibrated hot-wire data and mean flow computations show excellent agreement in the early stages of the transitional flow. However, examination of the wire Reynolds number and mass flux and total temperature eigenfunction profiles suggest that when operated in high overheat mode the sensitivity of the hot-wire to total temperature is significant. Thus, while uncalibrated hot-wire measurements are useful to characterize the overall features of the flow, calibrated hot-wire measurements are necessary for quantitative comparison with stability theory. Computations show that adverse pressure gradient and wall cooling decrease the boundary layer thickness and increase the frequency and amplification rate of the unstable second mode disturbances; these findings are consistent with the experimental observations.
Naiman, Hadassah. "Analysis and design of quiet hypersonic wind tunnels." 2010. http://hdl.rutgers.edu/1782.2/rucore10001600001.ETD.000052138.
Повний текст джерела(7399604), Phillip Portoni. "Using Suction for Laminar Flow Control in Hypersonic Quiet Wind Tunnels: A Feasibility Study." Thesis, 2019.
Знайти повний текст джерела(5930645), Kathryn A. Gray. "Flowfield Characterization of the Boeing/AFOSR Mach-6 Quiet Tunnel." Thesis, 2019.
Знайти повний текст джерелаHofferth, Jerrod William. "Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel." Thesis, 2013. http://hdl.handle.net/1969.1/150990.
Повний текст джерелаКниги з теми "Quiet Tunnels"
Wolf, Stephen W. D. Supersonic wind tunnel nozzles: A selected, annotated bibliography to aid in the development of quiet wind tunnel technology. Washington, D.C: National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаSchneider, Steven P. A quiet flow Ludwieg tube for study of transition in compressible boundary layers: Design and feasibility. West Lafayette, IN: School of Aeronautics and Astronautics, Purdue University, 1991.
Знайти повний текст джерелаSchneider, Steven P. Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаSchneider, Steven P. Supersonic quiet-tunnel development for laminar-turbulent transition research: Final report for NASA Langley grant NAG-1-1607. [Washington, DC: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаBarna, P. S. Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Progress report on the D.S.M.A. design. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. A quiet flow Ludwieg tube for study of transition in compressible boundary layers: Design and feasibility. [Washington, D.C: National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Development of Quiet-Flow Supersonic Wind Tunnels for Laminar-Turbulent Transition Research. Independently Published, 2018.
Знайти повний текст джерелаDevelopment of quiet-flow supersonic wind tunnels for laminar-turbulent transition research: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Supersonic quiet-tunnel development for laminar-turbulent transition research: Final report for NASA Langley grant NAG-1-1607. [Washington, DC: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаЧастини книг з теми "Quiet Tunnels"
Beckwith, Ivan E. "High-Speed Quiet Tunnels." In Advances in Soil Science, 49–51. New York, NY: Springer New York, 1990. http://dx.doi.org/10.1007/978-1-4612-3430-2_8.
Повний текст джерелаPate, Samuel R. "Dominance of “Noise” on Boundary Layer Transition in Conventional Wind Tunnels — a Place for the “Quiet” Ballistic Range in Future Studies." In Advances in Soil Science, 77–87. New York, NY: Springer New York, 1990. http://dx.doi.org/10.1007/978-1-4612-3430-2_11.
Повний текст джерелаShen, Junmou, Ying Zhang, Dan Wang, Ruiqu Li, and Jian Gong. "CFD Evaluation and Experiment Test of the Running Time of the Ludwieg Tube Quiet Wind Tunnel." In 31st International Symposium on Shock Waves 2, 221–30. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91017-8_27.
Повний текст джерелаXia, Dongrui, Lijiang Han, Yang Li, Lichuang Ma, and Junjie Yan. "Nonlinear Seismic Response Analysis of the Surrounding Rock-Tunnel System in the Mountain Areas Under SV Wave." In Advances in Transdisciplinary Engineering. IOS Press, 2021. http://dx.doi.org/10.3233/atde210185.
Повний текст джерелаDylan, Huw, David V. Gioe, and Michael S. Goodman. "A ‘Gangster Act’: The Berlin Tunnel." In The CIA and the Pursuit of Security, 54–63. Edinburgh University Press, 2020. http://dx.doi.org/10.3366/edinburgh/9781474428842.003.0003.
Повний текст джерелаLuo, Yifan, Matteo Toso, Bailu Si, Federico Stella, and Alessandro Treves. "Grid Cells Lose Coherence in Realistic Environments." In Hippocampus - Cytoarchitecture and Diseases. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.100310.
Повний текст джерелаDaub, Adrian. "The Ballad, the Public, and Gendered Community." In What the Ballad Knows, 211—C7.F1. Oxford University PressNew York, 2022. http://dx.doi.org/10.1093/oso/9780190885496.003.0008.
Повний текст джерелаRodden, John G. "After the Wall: Pride before the Fall, 1961–89." In Repainting the Little Red Schoolhouse. Oxford University Press, 2002. http://dx.doi.org/10.1093/oso/9780195112443.003.0011.
Повний текст джерелаBeris, Antony N., and Brian J. Edwards. "Symplectic Geometry in Optics." In Thermodynamics of Flowing Systems: with Internal Microstructure. Oxford University Press, 1994. http://dx.doi.org/10.1093/oso/9780195076943.003.0006.
Повний текст джерелаSchmickler, Wolfgang. "Theoretical considerations of electron-transfer reactions." In Interfacial Electrochemistry. Oxford University Press, 1996. http://dx.doi.org/10.1093/oso/9780195089325.003.0011.
Повний текст джерелаТези доповідей конференцій з теми "Quiet Tunnels"
Schneider, Steven. "The Development of Hypersonic Quiet Tunnels." In 37th AIAA Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-4486.
Повний текст джерелаLax, Philip, and Sergey B. Leonov. "Condensation-Limited Operational Maps of Notre Dame Large Quiet Tunnels." In AIAA SCITECH 2022 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-1719.
Повний текст джерелаSchneider, Steven P. "Developing Mechanism-Based Methods for Estimating Hypersonic Boundary-Layer Transition in Flight: The Role of Quiet Tunnels." In 43rd AIAA Fluid Dynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-2608.
Повний текст джерелаRedonnet, Stéphane, and Jean Bulte. "Numerical Investigation of the Refraction Effects by Jet Flows in Anechoic Wind Tunnels, with Application to NASA/LaRC Quiet Flow Facility." In 21st AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3268.
Повний текст джерелаHofferth, Jerrod, Rodney Bowersox, and William Saric. "The Mach 6 Quiet Tunnel at Texas A&M: Quiet Flow Performance." In 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-4794.
Повний текст джерелаBorg, Matthew, Steven Schneider, and Thomas Juliano. "Inlet Measurements and Quiet Flow Improvements in the Boeing/AFOSR Mach-6 Quiet Tunnel." In 44th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-1317.
Повний текст джерелаErdos, John, and Robert Bakos. "Prospects for a quiet hypervelocity shock-expansion tunnel." In 25th Plasmadynamics and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2500.
Повний текст джерелаWeiss, Julien, and Ndaona Chokani. "Quiet Tunnel Experiments of Shockwave / Turbulent Boundary Layer Interaction." In 36th AIAA Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3362.
Повний текст джерелаWILKINSON, S., S. ANDERS, F. J. CHEN, and I. BECKWITH. "Supersonic and hypersonic quiet tunnel technology at NASA Langley." In 28th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3908.
Повний текст джерелаSchneider, Steven, Shann Rufer, Craig Skoch, Erick Swanson, and Matthew Borg. "Instability and Transition in the Mach-6 Quiet Tunnel." In 34th AIAA Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-2247.
Повний текст джерелаЗвіти організацій з теми "Quiet Tunnels"
Grossir, 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 джерелаKnight, Doyle D., and Hadassah Naiman. Towards High-Reynolds Number Quiet Flow in Hypersonic Tunnels. Fort Belvoir, VA: Defense Technical Information Center, February 2009. http://dx.doi.org/10.21236/ada498212.
Повний текст джерелаSchneider, Steven P. Towards High-Reynolds-Number Quiet Flow in Hypersonic Wind Tunnels. Fort Belvoir, VA: Defense Technical Information Center, April 2009. http://dx.doi.org/10.21236/ada500049.
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 джерелаSegura, Rodrigo. Oscillations in a Forward-Facing Cavity Measured Using Laser-Differential Interferometry in a Hypersonic Quiet Tunnel. Fort Belvoir, VA: Defense Technical Information Center, December 2007. http://dx.doi.org/10.21236/ada474770.
Повний текст джерела