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Статті в журналах з теми "Transonic tunnel"
Greenwell, D. I. "Transonic industrial wind tunnel testing in the 2020s." Aeronautical Journal 126, no. 1295 (December 2, 2021): 125–51. http://dx.doi.org/10.1017/aer.2021.107.
Повний текст джерелаTsushima, Natsuki, Kenichi Saitoh, Hitoshi Arizono, and Kazuyuki Nakakita. "Structural and Aeroelastic Studies of Wing Model with Metal Additive Manufacturing for Transonic Wind Tunnel Test by NACA 0008 Example." Aerospace 8, no. 8 (July 25, 2021): 200. http://dx.doi.org/10.3390/aerospace8080200.
Повний текст джерелаQian, Wei, and De Guan. "The Design, Manufacture and Wind Tunnel Test of the Full Aircraft Transonic Flutter Model." Advanced Materials Research 487 (March 2012): 267–72. http://dx.doi.org/10.4028/www.scientific.net/amr.487.267.
Повний текст джерелаChen, Dan, Xiaosong Yang, Gang Li, Shouchun Guo, and Tianyi Chen. "Relativity Research of Total Pressure and Regulating Valve in Continuous Wind Tunnel and Its Application." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 38, no. 2 (April 2020): 325–32. http://dx.doi.org/10.1051/jnwpu/20203820325.
Повний текст джерелаKaczyński, P., R. Szwaba, M. Piotrowicz, P. Flaszyński, and P. Doerffer. "Wind tunnel investigations of aircraft airfoil in cruise conditions." Journal of Physics: Conference Series 2367, no. 1 (November 1, 2022): 012019. http://dx.doi.org/10.1088/1742-6596/2367/1/012019.
Повний текст джерелаKiock, R., F. Lehthaus, N. C. Baines, and C. H. Sieverding. "The Transonic Flow Through a Plane Turbine Cascade as Measured in Four European Wind Tunnels." Journal of Engineering for Gas Turbines and Power 108, no. 2 (April 1, 1986): 277–84. http://dx.doi.org/10.1115/1.3239900.
Повний текст джерелаBRUCE, P. J. K., D. M. F. BURTON, N. A. TITCHENER, and H. BABINSKY. "Corner effect and separation in transonic channel flows." Journal of Fluid Mechanics 679 (May 31, 2011): 247–62. http://dx.doi.org/10.1017/jfm.2011.135.
Повний текст джерелаDamljanović, Dijana, Đorđe Vuković, Goran Ocokoljić, and Boško Rašuo. "Convergence of transonic wind tunnel test results of the AGARD-B standard model." FME Transactions 48, no. 4 (2020): 761–69. http://dx.doi.org/10.5937/fme2004761d.
Повний текст джерелаPhillips, Pamela S., and Edgar G. Waggoner. "Transonic wind-tunnel wall interference prediction code." Journal of Aircraft 27, no. 11 (November 1990): 915–16. http://dx.doi.org/10.2514/3.45959.
Повний текст джерелаEdwards, John W. "National Transonic Facility Model and Tunnel Vibrations." Journal of Aircraft 46, no. 1 (January 2009): 46–52. http://dx.doi.org/10.2514/1.30080.
Повний текст джерелаДисертації з теми "Transonic tunnel"
Jones, Gregory Stephen. "The measurement of wind tunnel flow quality at transonic speeds." Diss., Virginia Tech, 1991. http://hdl.handle.net/10919/39109.
Повний текст джерелаPh. D.
Rosson, Joel Christopher. "Dynamic flow quality measurements in a transonic cryogenic wind tunnel." Thesis, Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/101463.
Повний текст джерелаM.S.
Neal, Graeme. "Three-dimensional model testing in the transonic self-streamlining wind tunnel." Thesis, University of Southampton, 1988. https://eprints.soton.ac.uk/52257/.
Повний текст джерелаGriffith, Dwaine O. "Turbulence measurements and noise generation in a transonic cryogenic wind tunnel." Thesis, Virginia Tech, 1989. http://hdl.handle.net/10919/45979.
Повний текст джерелаA high-frequency combination probe was used to measure dynamic flow quality in the test section of the NASA Langley 0.3-m Transonic Cryogenic Tunnel. The probe measures fluctuating stagnation (total) temperature and pressure, static pressure, and flow angles in two orthogonal planes. Simultaneous unsteady temperature and pressure measurements were also made in the settling chamber of the tunnel. The data show that the stagnation temperature fluctuations remain constant, and the stagnation pressure fluctuations increase by a factor of two, as the flow accelerates from the settling chamber to the test section. In the test section, the maximum rms value of the normalized fluctuating velocity is 0.7 percent. Correlation coefficients l failed to show vortlcity, entropy, or sound as the dominant mode of turbulence in the tunnel.
At certain tunnel operating conditions, periodic disturbances are seen in the data taken in the test section. A possible cause for the disturbances is found to be acoustic coupling of the test section and plenum chamber via the perforated side walls in the tunnel. The experimental data agree well with the acoustic coupling theory.
Master of Science
Suratanakavikul, Varangrat. "Computational study of compressible flow in an S-shaped duct." Thesis, Imperial College London, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.313370.
Повний текст джерелаJeffries, Michael. "Initial investigations of transonic turbine aerodynamics using the Carleton University high-speed wind tunnel." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2001. http://www.collectionscanada.ca/obj/s4/f2/dsk3/ftp04/NQ60956.pdf.
Повний текст джерелаBailey, Matthew Marlando. "An Extended Calibration and Validation of a Slotted-Wall Transonic Wall-Interference Correction Method for the National Transonic Facility." Diss., Virginia Tech, 2019. http://hdl.handle.net/10919/95882.
Повний текст джерелаDoctor of Philosophy
The purpose of conducting experimental tests in wind tunnels is often to acquire a quantitative measure of test article aerodynamic characteristics in such a way that those specific characteristics can be accurately translated into performance characteristics of the real vehicle that the test article intends to simulate. The difficulty in accurately simulating the real flow problem may not be readily apparent, but scientists and engineers have been working to improve this desired equivalence for the better part of the last half-century. The primary aspects of experimental aerodynamics simulation that present difficulty in attaining equivalence are: geometric fidelity, accurate scaling, and accounting for the presence of walls. The problem of scaling has been largely addressed by adequately matching conditions of similarity like compressibility (Mach number), and viscous effects (Reynolds number). However, accounting for the presence of walls in the experimental setup has presented ongoing challenges for ventilated boundaries; these challenges include difficulties in the correction process, but also extend into the determination of correction uncertainties. Exploiting a previously designed statistical validation method, this effort accomplishes the extension of a calibration and validation effort for a boundary pressure wall interference corrections method. The foundational calibration and validation work was based on blockage interference only, while this present work extends the assessment of the method to encompass blockage and lift interference production. The validation method involves the establishment of independent cases that are then compared to rigorously determine the degree to with the correction method can converge free-air solutions for differing interference scenarios. The process involved first establishing an empty-tunnel calibration to gain both a centerline Mach profile of the facility at various ventilation settings, and to gain a baseline wall pressure signature undisturbed by a test article. The wall boundary condition parameters were then calibrated with a blockage and lift interference producing test article, and final corrected performance coefficients were compared for varying test section ventilated configurations to validate the corrections process and assess its domain of applicability. During the validation process discrimination between homogeneous and discrete implementations of the boundary condition was accomplished and final results indicated comparative strength in the discrete implementation's ability to capture experimental flow physics. Final results indicate that a discrete implementation of the General Slotted Wall boundary condition is effective in significantly reducing variations caused by differing interference fields. Corrections performed with the discrete implementation of the boundary condition collapse differing measurements of lift coefficient to within 0.0027, drag coefficient to within 0.0002, and pitching moment coefficient to within 0.0020.
Hatchett, John Henry. "An Investigation of Effectiveness of Normal and Angled Slot Film Cooling in a Transonic Wind Tunnel." Thesis, Virginia Tech, 2008. http://hdl.handle.net/10919/31324.
Повний текст джерелаMaster of Science
Doig, Graham Mechanical & Manufacturing Engineering Faculty of Engineering UNSW. "Compressible ground effect aerodynamics." Awarded by:University of New South Wales. Mechanical & Manufacturing Engineering, 2009. http://handle.unsw.edu.au/1959.4/44696.
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 джерелаКниги з теми "Transonic tunnel"
Brooks, Cuyler W. The NASA Langley 8-Foot Transonic Pressure Tunnel calibration. Hampton, Va: Langley Research Center, 1994.
Знайти повний текст джерелаBrooks, Cuyler W. The NASA Langley 8-foot transonic pressure tunnel calibration. Hampton: National Aeronautics and Space Administration, Langley Research Center, 1994.
Знайти повний текст джерелаEverhart, Joel L. Slotted-wall flow-field measurements in a transonic wind tunnel. Hampton, Va: Langley Research Center, 1991.
Знайти повний текст джерелаCapone, Francis J. The NASA Langley 16-Foot Transonic Tunnel: Historical overview, facility description, calibration, flow characteristics, and test capabilities. Hampton, Va: Langley Research Center, 1995.
Знайти повний текст джерелаKuczka, Detlef. Hybridverfahren fur instationare Messungen in trassonischen Windkanalen am Beispiel der harmonischen Nickschwingung. Koln: DFVLR, 1988.
Знайти повний текст джерелаBruce, Robert A. A vapor generator for transonic flow visualization. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Знайти повний текст джерелаBruce, Robert A. A vapor generator for transonic flow visualization. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Знайти повний текст джерелаAl-Saadi, Jassim A. Wall interference and boundary simulation in a transonic wind tunnel with a discretely slotted test section. Hampton, Va: Langley Research Center, 1993.
Знайти повний текст джерелаGreen, Lawrence L. Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels. Hampton, Va: Langley Research Center, 1991.
Знайти повний текст джерелаSchairer, Edward T. A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Знайти повний текст джерелаЧастини книг з теми "Transonic tunnel"
Bolgar, Istvan, Sven Scharnowski, and Christian J. Kähler. "Effects of a Launcher’s External Flow on a Dual-Bell Nozzle Flow." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 115–27. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_7.
Повний текст джерелаBobbitt, Percy J., William D. Harvey, Charles D. Harris, and Cuyler W. Brooks. "The Langley 8-ft Transonic Pressure Tunnel Laminar-Flow-Control Experiment." In ICASE/NASA LaRC Series, 247–411. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2872-1_8.
Повний текст джерелаRasuo, Bosko. "On Boundary Layer Control in Two-Dimensional Transonic Wind Tunnel Testing." In Solid mechanics and its applications, 473–82. Dordrecht: Springer Netherlands, 2006. http://dx.doi.org/10.1007/978-1-4020-4150-1_46.
Повний текст джерелаMignosi, André, J. P. Archambaund, A. Seraudie, and J. B. Dor. "The T2 Cryogenic Transonic Wind Tunnel of Onera-Cert Toulouse France." In Advances in Cryogenic Engineering, 71–78. Boston, MA: Springer US, 1994. http://dx.doi.org/10.1007/978-1-4615-2522-6_8.
Повний текст джерелаCastro, Breno M., Kevin D. Jones, Max F. Platzer, Stefan Weber, and John A. Ekaterinaris. "Numerical Investigation of Transonic Flutter and Modeling of Wind Tunnel Interference Effects." In IUTAM Symposium Transsonicum IV, 71–78. Dordrecht: Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-010-0017-8_12.
Повний текст джерелаDor, J. B., A. Mignosi, A. Seraudie, and B. Benoit. "Wind Tunnel Studies of Natural Shock Wave — Separation Instabilities for Transonic Airfoil Tests." In Symposium Transsonicum III, 417–27. Berlin, Heidelberg: Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-83584-1_34.
Повний текст джерелаvon Geyr, H. Frhr, C. C. Rossow, and H. Hoheisel. "Influence of transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 475–82. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-39604-8_59.
Повний текст джерелаRichter, K., and H. Rosemann. "Numerical Simulation of Wind Tunnel Wall Effects on the Transonic Flow around an Airfoil Model." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 525–32. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-35680-3_62.
Повний текст джерелаChanetz, Bruno, Jean Délery, Patrick Gilliéron, Patrick Gnemmi, Erwin R. Gowree, and Philippe Perrier. "Transonic Wind Tunnels." In Springer Tracts in Mechanical Engineering, 97–113. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-35562-3_4.
Повний текст джерелаBruse, M., K. W. Bock, S. Tusche, and M. Jacobs. "Unsteady Measurements with the Continuously Rotating DLR-PSP-Model at the Transonic Wind Tunnel Göttingen (DNW-TWG)." In New Results in Numerical and Experimental Fluid Mechanics III, 103–10. Berlin, Heidelberg: Springer Berlin Heidelberg, 2002. http://dx.doi.org/10.1007/978-3-540-45466-3_13.
Повний текст джерелаТези доповідей конференцій з теми "Transonic tunnel"
BARNWELL, R., C. EDWARDS, R. KILGORE, and D. DRESS. "Optimum transonic wind tunnel." In 14th Aerodynamic Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-755.
Повний текст джерелаHelland, Stephen, and Courtney Henson. "Transonic Tunnel Comparison Test." In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-402.
Повний текст джерелаHergert, D., G. Smith, A. Krynytzky, and C. Jauch. "Transonic wind tunnel circuit upgrade." In 39th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-452.
Повний текст джерелаMarino, Antonello, and Aldo Bonfiglioli. "Optimization of the Porosity Distribution in Transonic Wind Tunnel." In ASME 2012 Fluids Engineering Division Summer Meeting collocated with the ASME 2012 Heat Transfer Summer Conference and the ASME 2012 10th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/fedsm2012-72487.
Повний текст джерелаCahill, David, Melissa Minter, and Richard Roberts. "FAVOR - National Transonic Wind Tunnel Comparison." In U.S. Air Force T&E Days 2010. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-1716.
Повний текст джерелаKrynytzky, Alexander, and Dennis Hergert. "Boeing Transonic Wind Tunnel Upgrade Assessment (Invited)." In 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-2782.
Повний текст джерелаEdwards, John, and John Edwards. "National Transonic Facility model and tunnel vibrations." In 35th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-345.
Повний текст джерелаChung, K., J. Miau, and J. Yieh. "Initial operation of ASTRC/NCKU transonic wind tunnel." In 25th Plasmadynamics and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2515.
Повний текст джерелаPHILLIPS, PAMELA, and EDGAR WAGGONER. "A transonic wind tunnel wall interference prediction code." In 6th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2538.
Повний текст джерелаCrowder, J., G. Amiryants, and V. Bounkov. "Flying strut traverser for transonic wind tunnel calibration." In 20th AIAA Advanced Measurement and Ground Testing Technology Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-2872.
Повний текст джерелаЗвіти організацій з теми "Transonic tunnel"
Lowry, Heard S., Mike S. Smith, William T. Bertrand, Fred Heltsley, and Daryl W. Sinclair. Integrated Optical Diagnostics for 16-ft Transonic Wind Tunnel. Fort Belvoir, VA: Defense Technical Information Center, February 2001. http://dx.doi.org/10.21236/ada387335.
Повний текст джерелаWong, J. K., G. N. Banks, and H. Whaley. Combustion evaluation of BP TRANSOIL emulsion in CCRL pilot-scale flame tunnel furnace. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 1989. http://dx.doi.org/10.4095/304426.
Повний текст джерела