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Статті в журналах з теми "Wind tunnel cascade test"
Kiock, 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 джерелаRona, Aldo, Renato Paciorri, and Marco Geron. "Design and Testing of a Transonic Linear Cascade Tunnel With Optimized Slotted Walls." Journal of Turbomachinery 128, no. 1 (June 23, 2005): 23–34. http://dx.doi.org/10.1115/1.2101856.
Повний текст джерелаZhang, Jian Guo, and Hui Min Zhuang. "Wind Tunnel Test of Tall Buildings with Irregularities of Elevation." Applied Mechanics and Materials 578-579 (July 2014): 1208–11. http://dx.doi.org/10.4028/www.scientific.net/amm.578-579.1208.
Повний текст джерелаBorovkov, Aleksei. "Efficiency Analysis of Blade Cascades of Axial Compressors by the Results of Wind Tunnel Test." Journal of Advanced Research in Dynamical and Control Systems 12, no. 01-Special Issue (February 13, 2020): 953–61. http://dx.doi.org/10.5373/jardcs/v12sp1/20201146.
Повний текст джерелаFořt, J., J. Fürst, J. Halama, V. Hric, P. Louda, M. Luxa, and D. Šimurda. "Numerical simulation of flow through cascade in wind tunnel test section and stand-alone configurations." Applied Mathematics and Computation 319 (February 2018): 633–46. http://dx.doi.org/10.1016/j.amc.2017.07.040.
Повний текст джерелаHake, Leander, Felix Reinker, Robert Wagner, Stefan aus der Wiesche, and Markus Schatz. "The Profile Loss of Additive Manufactured Blades for Organic Rankine Cycle Turbines." International Journal of Turbomachinery, Propulsion and Power 7, no. 1 (March 21, 2022): 11. http://dx.doi.org/10.3390/ijtpp7010011.
Повний текст джерелаNiehuis, Reinhard, and Martin Bitter. "The High-Speed Cascade Wind Tunnel at the Bundeswehr University Munich after a Major Revision and Upgrade." International Journal of Turbomachinery, Propulsion and Power 6, no. 4 (October 29, 2021): 41. http://dx.doi.org/10.3390/ijtpp6040041.
Повний текст джерелаRechter, H., W. Steinert, and K. Lehmann. "Comparison of Controlled Diffusion Airfoils With Conventional NACA 65 Airfoils Developed for Stator Blade Application in a Multistage Axial Compressor." Journal of Engineering for Gas Turbines and Power 107, no. 2 (April 1, 1985): 494–98. http://dx.doi.org/10.1115/1.3239758.
Повний текст джерелаTweedt, D. L., H. A. Schreiber, and H. Starken. "Experimental Investigation of the Performance of a Supersonic Compressor Cascade." Journal of Turbomachinery 110, no. 4 (October 1, 1988): 456–66. http://dx.doi.org/10.1115/1.3262219.
Повний текст джерелаVlček, Václav, and Pavel Procházka. "Test section of the wind tunnel IT for aeroelastic experiments with blade cascades." EPJ Web of Conferences 213 (2019): 02095. http://dx.doi.org/10.1051/epjconf/201921302095.
Повний текст джерелаДисертації з теми "Wind tunnel cascade test"
Baydar, Adem. "Hot-wire measurements of compressor blade wakes in a cascade wind tunnel/." Thesis, Monterey, California. Naval Postgraduate School, 1988. http://hdl.handle.net/10945/23254.
Повний текст джерелаHamilton, Christianne Rhea. "Design of Test Sections for a High Enthalpy Wind Tunnel." MSSTATE, 2003. http://sun.library.msstate.edu/ETD-db/theses/available/etd-04082003-114126/.
Повний текст джерелаSparks, Russell. "A novel six degree of freedom dynamic wind tunnel test facility." Thesis, University of Manchester, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.492066.
Повний текст джерелаMurray, Kenneth Douglas. "Automation and extension of LDV measurements of off-design flow in a cascade wind tunnel." Thesis, Monterey, California. Naval Postgraduate School, 1989. http://hdl.handle.net/10945/25708.
Повний текст джерелаTourn, Cremona Silvana Cecilia. "Characterization of a New Open Jet Wind Tunnel to Optimize and Test Vertical Axis Wind Turbines." Doctoral thesis, Universitat Rovira i Virgili, 2017. http://hdl.handle.net/10803/461079.
Повний текст джерелаBasado en el creciente interés en las tecnologías ambientales urbanas, el estudio de turinas de eje vertical de pequeña escala muestra desafíos motivadores. En esta tesis, se presentan los criterios de diseño, las características y potencialidades de un nuevo túnel de viento de seccion de prueba abierta. Tiene un área de salida e la boquilla del túnel de 1,5 x 1,5 m2, y se puede operar con velocidades de salida de 3 m/s a 17 m/s. La caracterización del flujo se ha llevado a cabo con tubos pitot calibrados, anemómetros de cazoletas y anemómetros de hilo caliente. Se consideran dos configuraciones diferentes del área de prueba, con y sin techo. Las mediciones en el rango de velocidades de salida disponibles muestran que la sección transversal, donde las intensidades de velocidad y turbulencia muestran un nivel aceptable de uniformidad, tiene un área de 0,8 x 0,8 m2 y una dimensión de 2 m desde la salida de la boquilla del túnel. En esta sección de trabajo, la intensidad máxima de la turbulencia es del 4%. La caracterización detallada del flujo realizado indica que el túnel de viento se puede utilizar para probar modelos a de aerogeneradores de pequeña escala.
Based on the increasing interest in urban environmental technologies, the study of small scale vertical axis wind turbines shows motivating challenges. In this thesis, we present the design criteria, characteristics and potentials of a new open jet wind tunnel. It has a nozzle exit area of 1.5 x1.5 m2, and it can be operated with exit velocities from 3 m/s to 17 m/s. The characterization of the flow has been carried out with calibrated pitot tubes, cup anemometers, and hot wire anemometers. Two different configurations of the test area, with and without a ceiling, are considered. Measurements in the range of available exit velocities show that the cross section, where the velocity and turbulence intensities show an acceptable level of uniformity, has an area of 0.8 x 0.8 m2 and a streamwise dimension of 2 m from the nozzle exit of the tunnel. In this working section, the maximum turbulence intensity is 4%. The detailed characterization of the flow carried out indicates that the wind tunnel can be used to test small scale models of wind turbines.
Dalley, Sam. "Wind tunnel measurements on a low rise building and comparison with full-scale." Thesis, University of Surrey, 1993. http://epubs.surrey.ac.uk/886/.
Повний текст джерелаCapasso, Michael Anthony. "Construction and wind tunnel test of a 1/12th scale helicopter model." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1994. http://handle.dtic.mil/100.2/ADA288487.
Повний текст джерелаHamm, Christopher Eric. "AN ASSESSMENT OF FLOW QUALITY IN AN OPEN TEST SECTION WIND TUNNEL." MSSTATE, 2009. http://sun.library.msstate.edu/ETD-db/theses/available/etd-11022009-115210/.
Повний текст джерелаJames, Ralph William. "The effect of boundary layer blowing in the corner region of a linear compressor cascade wind tunnel." Thesis, This resource online, 1995. http://scholar.lib.vt.edu/theses/available/etd-05092009-040547/.
Повний текст джерелаMuthanna, Chittiappa. "The Effects of Free Stream Turbulence on the Flow Field through a Compressor Cascade." Diss., Virginia Tech, 2002. http://hdl.handle.net/10919/28753.
Повний текст джерелаPh. D.
Книги з теми "Wind tunnel cascade test"
Norris, R. B. The flying wind tunnel. New York: AIAA, 1989.
Знайти повний текст джерелаB, Kelley P., and United States. National Aeronautics and Space Administration, eds. Wind tunnel test IA300 analysis and results. Huntsville, AL: Lockheed Missiles & Space Co., Huntsville Engineering Center, 1987.
Знайти повний текст джерелаK, Wailes W., and Ames Research Center, eds. Advanced recovery systems wind tunnel test report. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Знайти повний текст джерелаKeas, Paul. SOFIA II model telescope and wind tunnel test. [Moffett Field, Calif.]: NASA Ames Research Center, 1995.
Знайти повний текст джерелаBaydar, Adem. Hot-wire measurements of compressor blade wakes in a cascade wind tunnel. Monterey, California: Naval Postgraduate School, 1988.
Знайти повний текст джерелаKelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Знайти повний текст джерелаK, Abeyounis W., and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Знайти повний текст джерелаKelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Знайти повний текст джерелаOhman, L. H. New transonic test sections for the NAE 5ftx5ft trisonic wind tunnel. Ottawa: National Aeronautical Establishment, 1990.
Знайти повний текст джерелаRandall, Peterson, and Ames Research Center, eds. Shake test results of the MDHC test stand in the 40- by 80-foot wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Знайти повний текст джерелаЧастини книг з теми "Wind tunnel cascade test"
Gao, Lei. "Wind Tunnel Test." In Encyclopedia of Ocean Engineering, 1–4. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-10-6963-5_265-1.
Повний текст джерелаGao, Lei. "Wind Tunnel Test." In Encyclopedia of Ocean Engineering, 2169–72. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-10-6946-8_265.
Повний текст джерелаChanetz, Bruno, Jean Délery, Patrick Gilliéron, Patrick Gnemmi, Erwin R. Gowree, and Philippe Perrier. "Computer-Aided Wind Tunnel Test and Analysis." In Springer Tracts in Mechanical Engineering, 273–83. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-35562-3_13.
Повний текст джерелаLu, Zheng, Sami F. Masri, and Xilin Lu. "Wind Tunnel Test Study on Particle Damping Technology." In Particle Damping Technology Based Structural Control, 225–91. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-3499-7_7.
Повний текст джерелаLiu, Jin, Yuhui Song, and Jing Hu. "Investigation on Dynamic Derivative Test Technique in Hypersonic Wind Tunnel." In Lecture Notes in Electrical Engineering, 883–91. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_69.
Повний текст джерелаYang, Lung-Jieh, Hsi-Chun Lee, Ai-Lien Feng, Chien-Wei Chen, Jenmu Wang, Yuan-Lung Lo, and Chia-Kuo Wang. "The Wind Tunnel Test and Unsteady CFD of an Ornithopter Formation." In Lecture Notes in Mechanical Engineering, 9–16. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-1771-1_4.
Повний текст джерелаAraszkiewicz, Piotr. "Use of Rapid Manufacturing Methods for Creating Wind Tunnel Test Models." In Lecture Notes in Mechanical Engineering, 36–43. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-04975-1_5.
Повний текст джерелаGao, Liqiang, Xiong Hu, Dejian Sun, Ying Xi, and Guohua Wang. "Numerical Simulation and Wind Tunnel Test Validation of the Aerodynamic Brake Panel." In Advances in Mechanical Design, 911–21. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-6553-8_61.
Повний текст джерелаHou, Yingyu, and Ziqiang Liu. "Aeroelastic Test of Large Flexible Structure Based on Electromagnetic Dry Wind Tunnel." In Lecture Notes in Electrical Engineering, 2684–91. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_215.
Повний текст джерелаStreit, Thomas, Heiko Geyr von Schweppenburg, David Cruz, and Rafael Sanchez. "DLR Feasibility Study of HLFC Wing Designs for S1MA Wind Tunnel Test." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 235–45. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-79561-0_23.
Повний текст джерелаТези доповідей конференцій з теми "Wind tunnel cascade test"
Kiock, 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." In ASME 1985 Beijing International Gas Turbine Symposium and Exposition. American Society of Mechanical Engineers, 1985. http://dx.doi.org/10.1115/85-igt-44.
Повний текст джерелаWagner, Robert, Kai Dönnebrink, Felix Reinker, Karsten Hasselmann, Jonas Rejek, and Stefan aus der Wiesche. "A Modular Low-Speed Wind Tunnel With Two Test Sections and Variable Inflow Angle." In ASME 2015 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/imece2015-50232.
Повний текст джерелаBrunner, Stefan, Leonhard Fottner, and Heinz-Peter Schiffer. "Comparison of Two Highly Loaded Low Pressure Turbine Cascades Under the Influence of Wake-Induced Transition." In ASME Turbo Expo 2000: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/2000-gt-0268.
Повний текст джерелаMunoz Lopez, Edwin J., Alexander Hergt, and Sebastian Grund. "The New Chapter of Transonic Compressor Cascade Design at the DLR." In ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/gt2022-80189.
Повний текст джерелаGraiff, Mattia, Marian Staggl, Emil Göttlich, and Christian Wakelam. "Design and Evaluation of a Flow Capturing Device for a High-Speed Wind Tunnel." In ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gt2021-58667.
Повний текст джерелаHasselmann, Karsten, Felix Reinker, Stefan aus der Wiesche, Eugeny Y. Kenig, Frithjof Dubberke, and Jadran Vrabec. "Performance Predictions of Axial Turbines for Organic Rankine Cycle (ORC) Applications Based on Measurements of the Flow Through Two-Dimensional Cascades of Blades." In ASME 2014 Power Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/power2014-32098.
Повний текст джерелаSieverding, C. H., and T. Arts. "The VKI Compression Tube Annular Cascade Facility CT3." In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-336.
Повний текст джерелаGonzalez, Carlos R., Guillaume F. Bidan, Jason W. Bitting, Christopher M. Foreman, Jean-Philippe Junca-Laplace, Kevin D. Wood, and Dimitris E. Nikitopoulos. "Design, Characterization, and Verification of a Closed Loop Wind Tunnel With Linear Cascade and Upstream Wake Generator." In ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gt2015-42999.
Повний текст джерелаaus der Wiesche, Stefan, Felix Reinker, Robert Wagner, Leander Hake, and Max Passmann. "Critical and Choking Mach Numbers for Organic Vapor Flows Through Turbine Cascades." In ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gt2021-59013.
Повний текст джерелаRona, A., and J. P. Gostelow. "Performance Margins of Non-Reflecting Slotted Walls in a Transonic Linear Cascade Tunnel." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-91057.
Повний текст джерелаЗвіти організацій з теми "Wind tunnel cascade test"
Lammert, Michael P., Kenneth J. Kelly, and Janet Yanowitz. Correlations of Platooning Track Test and Wind Tunnel Data. Office of Scientific and Technical Information (OSTI), February 2018. http://dx.doi.org/10.2172/1422885.
Повний текст джерелаParker, M. J., and R. P. Addis. Wind tunnel test of Teledyne Geotech model 1564B cup anemometer. Office of Scientific and Technical Information (OSTI), April 1991. http://dx.doi.org/10.2172/5825677.
Повний текст джерелаHand, M. M., D. A. Simms, L. J. Fingersh, D. W. Jager, J. R. Cotrell, S. Schreck, and S. M. Larwood. Unsteady Aerodynamics Experiment Phase VI: Wind Tunnel Test Configurations and Available Data Campaigns. Office of Scientific and Technical Information (OSTI), December 2001. http://dx.doi.org/10.2172/15000240.
Повний текст джерелаSteinle, Frank W., Booth Jr., Rhew Dennis, and Ray D. Determination of Anelastic-Induced Error in Wind Tunnel Test Force and Moment Measurements. Fort Belvoir, VA: Defense Technical Information Center, January 1999. http://dx.doi.org/10.21236/ada370968.
Повний текст джерелаGillard, William J. Innovative Control Effectors (Configuration 101) Dynamic Wind Tunnel Test Report. Rotary Balance and Forced Oscillation Tests. Fort Belvoir, VA: Defense Technical Information Center, July 1998. http://dx.doi.org/10.21236/ada362903.
Повний текст джерелаLau, Benton H., Nicole Obriecht, Tanner Gasow, Brandon Hagerty, Kelly C. Cheng, and Ben W. Sim. Boeing-SMART Rotor Wind Tunnel Test Data Report for DARPA Helicopter Quieting Program (HQP), Phase 1B. Fort Belvoir, VA: Defense Technical Information Center, September 2010. http://dx.doi.org/10.21236/ada532806.
Повний текст джерелаClark, E. L. Error propagation equations and tables for estimating the uncertainty in high-speed wind tunnel test results. Office of Scientific and Technical Information (OSTI), August 1993. http://dx.doi.org/10.2172/10178382.
Повний текст джерелаVocke, Robert III D., and Gerardo Nunez. Test Data Report, Low-Speed Wind Tunnel Drag Test of a 2/5 Scale Lockheed AH-56 Cheyenne Door-Hinge Hub. Fort Belvoir, VA: Defense Technical Information Center, July 2016. http://dx.doi.org/10.21236/ad1011994.
Повний текст джерелаDodson, Michael G. An Historical and Applied Aerodynamic Study of the Wright Brothers' Wind Tunnel Test Program and Application to Successful Manned Flight. Fort Belvoir, VA: Defense Technical Information Center, May 2005. http://dx.doi.org/10.21236/ada437187.
Повний текст джерелаYeager, William T., Noonan Jr., Singleton Kevin W., Wilbur Jeffrey D., and Matthew L. Performance and Vibratory Loads Data from a Wind-Tunnel Test of a Model Helicopter Main-Rotor Blade with a Paddle-Type Tip. Fort Belvoir, VA: Defense Technical Information Center, May 1997. http://dx.doi.org/10.21236/ada406400.
Повний текст джерела