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Статті в журналах з теми "Wind tunnel balance"
Hasan, 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 джерелаVukovic, Djordje, and Dijana Damljanovic. "Thermal effects influencing measurements in a supersonic blowdown wind tunnel." Thermal Science 20, no. 6 (2016): 2101–12. http://dx.doi.org/10.2298/tsci160404175v.
Повний текст джерелаBurns, Devin E., and Peter A. Parker. "Additively Manufactured Wind-Tunnel Balance." Journal of Aircraft 57, no. 5 (September 2020): 958–63. http://dx.doi.org/10.2514/1.c035889.
Повний текст джерелаWANG, Wenjun, Hiroshi KUROYANAGI, and Kazunori YOSHIDA. "1A16 6 Force Component Balance for Wind Tunnel Model Tests." Proceedings of the Symposium on the Motion and Vibration Control 2010 (2010): _1A16–1_—_1A16–7_. http://dx.doi.org/10.1299/jsmemovic.2010._1a16-1_.
Повний текст джерелаEwald, B. "The accuracy of internal wind tunnel balances for wind tunnel force measurements, the problem of definition and verification." Aeronautical Journal 105, no. 1050 (August 2001): 443–49. http://dx.doi.org/10.1017/s0001924000012422.
Повний текст джерелаEWALD, B. "WIND TUNNEL INSTRUMENTATION TECHNIQUE BALANCE DESIGN PROBLEMS." International Conference on Aerospace Sciences and Aviation Technology 1, CONFERENCE (May 1, 1985): 1–8. http://dx.doi.org/10.21608/asat.1985.26474.
Повний текст джерелаKrajček Nikolić, Karolina, Anita Domitrović, and Slobodan Janković. "Estimation of Aerodynamic Coefficients in a Small Subsonic Wind Tunnel." PROMET - Traffic&Transportation 30, no. 4 (September 10, 2018): 457–63. http://dx.doi.org/10.7307/ptt.v30i4.2685.
Повний текст джерелаShi, Pengtao, Jihai Liu, Yingsong Gu, Zhichun Yang, and Pier Marzocca. "Full-Span Flying Wing Wind Tunnel Test: A Body Freedom Flutter Study." Fluids 5, no. 1 (March 16, 2020): 34. http://dx.doi.org/10.3390/fluids5010034.
Повний текст джерелаLynn, Keith C., Sean A. Commo, and Peter A. Parker. "Wind-Tunnel Force Balance Characterization for Hypersonic Research Applications." Journal of Aircraft 49, no. 2 (March 2012): 556–65. http://dx.doi.org/10.2514/1.c031567.
Повний текст джерелаLandman, Drew, Kenneth G. Toro, Sean A. Commo, and Keith C. Lynn. "Prediction Interval Development for Wind-Tunnel Balance Check-Loading." Journal of Aircraft 52, no. 3 (May 2015): 884–89. http://dx.doi.org/10.2514/1.c032930.
Повний текст джерелаДисертації з теми "Wind tunnel balance"
Katirci, Argun. "Automation And Verification Of Ankara Wind Tunnel." Master's thesis, METU, 2003. http://etd.lib.metu.edu.tr/upload/12607692/index.pdf.
Повний текст джерелаs test that was performed at NASA Langley Research Center.
Kayisoglu, Bengi. "Investigation Of Wind Effects On Tall Buildings Through Wind Tunnel Testing." Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613324/index.pdf.
Повний текст джерелаParker, David Huw. "Techniques for extreme attitude suspension of a wind tunnel model in a magnetic suspension and balance system." Thesis, University of Southampton, 1989. https://eprints.soton.ac.uk/52256/.
Повний текст джерелаEdwards, Alex T. "Comparison of Strain Gage and Fiber Optic Sensors On A Sting Balance In A Supersonic Wind Tunnel." Thesis, Virginia Tech, 2000. http://hdl.handle.net/10919/30799.
Повний текст джерела
This thesis considers an initial trial application of new fiber optic sensors on a conventional, six-component sting balance while retaining the original foil strain gage sensors for comparison. Tests were conducted with a blunt, 10º half-angle cone model in the Virginia Tech 9x9 inch Supersonic Wind Tunnel at Mach 2.4 with a total pressure of 48 psia and ambient total temperature of 25.3ºC. Results showed a close comparison between the foil strain gages and the fiber optic sensor measurements, which were set up to measure the normal force and pitching moment on the blunt cone model. A Finite Element Model (FEM) of the sting balance was produced in order to determine the best locations for the fiber optic sensors on the sting balance. Computational Fluid Dynamics (CFD) was also used in order to predict and compare the results acquired from all of the sensors.
Master of Science
Lines, Philipp A. "Upgrade of a LabVIEW based data acquisition system for wind tunnel test of a 1/10 scale OH-6A helicopter fuselage." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03Jun%5FLines.pdf.
Повний текст джерелаThesis advisor(s): E. Roberts Wood, Richard M. Howard. Includes bibliographical references (p. 53-54). Also available online.
Nacakli, Yavuz. "Detailed Measurements Of Dynamic Stability Derivatives Under Roll Oscillations For Standard Dynamic Model In Ankara Wind Tunnel." Master's thesis, METU, 2003. http://etd.lib.metu.edu.tr/upload/4/1206846/index.pdf.
Повний текст джерелаFryšták, Lukáš. "Aerodynamická optimalizace monopostu formule SAE." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2016. http://www.nusl.cz/ntk/nusl-254335.
Повний текст джерелаBroughton, Benjamin Albert. "Low speed wind tunnel testing and data correction methods for aircraft models in ground effect." Diss., University of Pretoria, 1999. http://hdl.handle.net/2263/24292.
Повний текст джерелаDissertation (MEng)--University of Pretoria, 1999.
Mechanical and Aeronautical Engineering
unrestricted
Sevier, Abigail. "Feasibility Study for Testing the Dynamic Stability of Blunt Bodies with a Magnetic Suspension System in a Supersonic Wind Tunnel." Case Western Reserve University School of Graduate Studies / OhioLINK, 2017. http://rave.ohiolink.edu/etdc/view?acc_num=case1493207020743959.
Повний текст джерелаChen, Ru-Ching. "Development of a Supersonic Nozzle and Test Section for use with a Magnetic Suspension System for Re-Entry Aeroshell Models." Case Western Reserve University School of Graduate Studies / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=case1544179612537658.
Повний текст джерелаКниги з теми "Wind tunnel balance"
Britcher, Colin P. Application of magnetic suspension and balance systems to ultra-high Reynolds number facilities. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаBritcher, Colin P. Applications of magnetic suspension technology to large scale facilities: Progress, problems and promises. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаJohnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. Hampton, Va: Langley Research Center, 1989.
Знайти повний текст джерелаJohnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаJohnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаJohnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаJohnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаBaljeu, J. F. Development of a multi-component internal strain-gauge balance for model tests in a cryogenic wind tunnel. Amsterdam: National Aerospace Laboratory, 1988.
Знайти повний текст джерелаWelsh, B. L. A dynamic balance for the measurement of time-dependent aerodynamic forces on wind-tunnel models. London: HMSO, 1990.
Знайти повний текст джерелаHuebner, Lawrence D. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. Hampton, Va: Langley Research Center, 1993.
Знайти повний текст джерелаЧастини книг з теми "Wind tunnel balance"
Oyama, Tomokazu, T. Ichige, A. Inoue, and J. Bredenbeck. "Electrical wind tunnel external balance system." In Proceedings, 1177–91. Wiesbaden: Springer Fachmedien Wiesbaden, 2014. http://dx.doi.org/10.1007/978-3-658-05130-3_84.
Повний текст джерелаHufnagel, Klaus. "Utilization of Balances in the Wind Tunnel." In Experimental Fluid Mechanics, 273–76. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-97766-5_10.
Повний текст джерелаŞtefănescu, Dan Mihai. "Strain Gauge Balances for Testing Car and Flight Models in Wind Tunnel Applications." In Handbook of Force Transducers, 177–88. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-35322-3_17.
Повний текст джерелаGonzalez, Miguel, Jose Miguel Ezquerro, Victoria Lapuerta, Ana Laveron, and Jacobo Rodriguez. "Components of a Wind Tunnel Balance: Design and Calibration." In Wind Tunnels and Experimental Fluid Dynamics Research. InTech, 2011. http://dx.doi.org/10.5772/21095.
Повний текст джерела"Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091A-2020)." In Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091A-2020). 12700 Sunrise Valley Drive, Suite 200, Reston, VA 20191: American Institute of Aeronautics and Astronautics, Inc., 2020. http://dx.doi.org/10.2514/4.106019.001.
Повний текст джерела"Recommended Practice: Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091-2003)." In Recommended Practice: Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091-2003). Washington, DC: American Institute of Aeronautics and Astronautics, Inc., 2003. http://dx.doi.org/10.2514/4.476464.001.
Повний текст джерелаТези доповідей конференцій з теми "Wind tunnel balance"
Alves, Leonardo Boa Sorte, Marco Gabaldo, Luiz Severiano Dutra, and Jose Eduardo Mautone Barros. "Wind Tunnel Balance." In 26th SAE BRASIL Inernational Congress and Display. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2017. http://dx.doi.org/10.4271/2017-36-0237.
Повний текст джерелаHufnagel, Klaus, Bernd Ewald, Ruediger Rebstock, and Junnai Zhai. "Advanced half model wind tunnel balance developments." In 21st Aerodynamic Measurement Technology and Ground Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-2385.
Повний текст джерелаKarkehabadi, Reza, and Ray Rhew. "Structural Integrity of a Wind Tunnel Balance." In 42nd AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-1293.
Повний текст джерелаLandman, Drew, and Jim Simpson. "A Wind Tunnel External Balance Calibration Using Design of Experiments." In 2007 U.S. Air Force T&E Days. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-1604.
Повний текст джерелаPolansky, L., W. Matich, and J. T. Kutney. "A New Multi-Component-Wind-Tunnel-Balance for Automotive Windtunnels." In International Congress & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1995. http://dx.doi.org/10.4271/950995.
Повний текст джерелаReis, Maria Luísa, Olympio Mello, and Sadahaki Uyeno. "Calibration Uncertainty of an External Six-Component Wind Tunnel Balance." In 33rd AIAA Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-3884.
Повний текст джерелаReis, Maria Luísa, Wilson Vieira, Itamar Barbosa, Olympio Achilles Mello, and Luciano Santos. "Validation of an External Six-Component Wind Tunnel Balance Calibration." In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-2300.
Повний текст джерелаChoi, Simon, and J. Stewart. "Force Balance Measurement Sensor in Wind Tunnel Aerodynamic Testing Environments." In USAF Developmental Test and Evaluation Summit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-6812.
Повний текст джерелаUlbrich, Norbert. "Combined Load Diagram for a Wind Tunnel Strain-Gage Balance." In 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-4203.
Повний текст джерелаBritcher, Colin P., and David E. Cox. "Electromagnetic Modeling of Wind Tunnel Magnetic Suspension and Balance Systems." In AIAA SCITECH 2023 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-1819.
Повний текст джерелаЗвіти організацій з теми "Wind tunnel balance"
Gillard, 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 джерелаFuchs, Marcel, Jerry Hatfield, Amos Hadas, and Rami Keren. Reducing Evaporation from Cultivated Soils by Mulching with Crop Residues and Stabilized Soil Aggregates. United States Department of Agriculture, 1993. http://dx.doi.org/10.32747/1993.7568086.bard.
Повний текст джерела