Literatura académica sobre el tema "Aerodynamic angle"
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Artículos de revistas sobre el tema "Aerodynamic angle"
Tripathi, Manish, Mahesh M. Sucheendran y Ajay Misra. "Experimental analysis of cell pattern on grid fin aerodynamics in subsonic flow". Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 234, n.º 3 (5 de septiembre de 2019): 537–62. http://dx.doi.org/10.1177/0954410019872349.
Texto completoSun, Xiao-Ying, Tian-E. Li, Guo-Chang Lin y Yue Wu. "A study on the aerodynamic characteristics of a stratospheric airship in its entire flight envelope". Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, n.º 5 (2 de agosto de 2017): 902–21. http://dx.doi.org/10.1177/0954410017723358.
Texto completoTaiming, Huang, Zhuang Xiaodong, Wan Zhongmin y Gu Zhengqi. "Experimental and numerical investigations of the vehicle aerodynamic drag with single-channel rear diffuser". Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering 234, n.º 8 (7 de febrero de 2020): 2216–27. http://dx.doi.org/10.1177/0954407019893849.
Texto completoBaigang, Mi y Yu Jingyi. "An Improved Nonlinear Aerodynamic Derivative Model of Aircraft at High Angles of Attack". International Journal of Aerospace Engineering 2021 (8 de septiembre de 2021): 1–12. http://dx.doi.org/10.1155/2021/5815167.
Texto completoXiang, Jinwu, Kai Liu, Daochun Li, Chunxiao Cheng y Enlai Sha. "Unsteady aerodynamic characteristics of a morphing wing". Aircraft Engineering and Aerospace Technology 91, n.º 1 (7 de enero de 2018): 1–9. http://dx.doi.org/10.1108/aeat-04-2017-0101.
Texto completoHu, Haode y Dongli Ma. "Airfoil Aerodynamics in Proximity to Wavy Ground for a Wide Range of Angles of Attack". Applied Sciences 10, n.º 19 (27 de septiembre de 2020): 6773. http://dx.doi.org/10.3390/app10196773.
Texto completoZhang, Yanqi y Zhaoming Zhang. "Unsteady Aerodynamic Characteristics of Antenna Rotating in Different Elevation Angles". International Journal of Antennas and Propagation 2021 (26 de julio de 2021): 1–16. http://dx.doi.org/10.1155/2021/5503330.
Texto completoWang, Xu, Yuanhao Qian, Zengshun Chen, Xiao Zhou, Huaqiang Li y Hailin Huang. "Numerical studies on aerodynamics of high-speed railway train subjected to strong crosswind". Advances in Mechanical Engineering 11, n.º 11 (noviembre de 2019): 168781401988727. http://dx.doi.org/10.1177/1687814019887270.
Texto completoHUANG, DA y GENXIN WU. "INVESTIGATION OF SUITABILITY FOR THE LINEAR SUPERPOSITION MODEL". Modern Physics Letters B 19, n.º 28n29 (20 de diciembre de 2005): 1631–34. http://dx.doi.org/10.1142/s0217984905010086.
Texto completoKang, Chang-kwon y Wei Shyy. "Analytical model for instantaneous lift and shape deformation of an insect-scale flapping wing in hover". Journal of The Royal Society Interface 11, n.º 101 (6 de diciembre de 2014): 20140933. http://dx.doi.org/10.1098/rsif.2014.0933.
Texto completoTesis sobre el tema "Aerodynamic angle"
Wilks, Brett Landon Burkhalter Johnny Evans. "Aerodynamics of wrap-around fins in supersonic flow". Auburn, Ala., 2005. http://repo.lib.auburn.edu/2005%20Fall/Thesis/WILKS_BRETT_54.pdf.
Texto completoFan, Yigang. "Identification of an Unsteady Aerodynamic Model up to High Angle of Attack Regime". Diss., Virginia Tech, 1997. http://hdl.handle.net/10919/29830.
Texto completoPh. D.
Stagg, Gregory A. "An Aerodynamic Model for Use in the High Angle of Attack Regime". Thesis, Virginia Tech, 1998. http://hdl.handle.net/10919/35596.
Texto completoMaster of Science
Sirangu, Vijaya. "AERODYNAMIC CONTROL OF SLENDER BODIES AT HIGH ANGLES OF ATTACK". University of Toledo / OhioLINK, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1271365316.
Texto completoSor, Wei Lun. "Aerodynamic Validation of Emerging Projectile Configurations". Thesis, Monterey, California. Naval Postgraduate School, 2012.
Buscar texto completoEver-increasing demands for accuracy and range in modern warfare have expedited the optimization of projectile design. The crux of projectile design lies in the understanding of its aerodynamic properties early in the design phase. This research first investigated the aerodynamic properties of a standard M549, 155mm projectile. The transonic speed region was the focus of the research as significant aerodynamic variation occurs within this particular region. Aerodynamic data from wind tunnel and range testing was benchmarked against modern aerodynamic prediction programs like ANSYS CFX and Aero-Prediction 09 (AP09). Next, a comparison was made between two types of angle of attack generation methods in ANSYS CFX. The research then focused on controlled tilting of the projectile’s nose to investigate the resulting aerodynamic effects. ANSYS CFX was found to provide better agreement with the experimental data than AP09.
Takahama, Morio, Noboru Sakamoto y Yuhei Yamato. "Attitude Stabilization of an Aircraft via Nonlinear Optimal Control Based on Aerodynamic Data". Institute of Electrical and Electronics Engineers, 2009. http://hdl.handle.net/2237/14420.
Texto completoMohmad, Rouyan Nurhana. "Model simulation suitable for an aircraft at high angle of attack". Thesis, Cranfield University, 2016. http://dspace.lib.cranfield.ac.uk/handle/1826/9722.
Texto completoQuickel, Reuben Alexander. "Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes". Thesis, Virginia Tech, 2019. http://hdl.handle.net/10919/89952.
Texto completoMaster of Science
Accurately measuring the total temperature of a high-speed fluid flow is a challenging task that is required in many research areas and industry applications. Many methods exist for measuring total temperature, but the use of thermocouple based probes immersed into a flow remains a common and desirable measurement technique. The difficulty in using thermocouple based probes to acquire total temperature stems from attempting to minimize or accurately predict the probe’s measurement error. Conduction, convection, and radiation heat transfer between the fluid flow and probe create challenges for minimizing measurement error so that the accurate total temperature can be obtained. Numerous studies have been performed in prior literature to account for simple cases of each error source. However, there are many complex, practical applications in which the influence of each error source has not been studied. The impacts of a freestream flow angle and the total temperature probe’s mounting structure have not been previously modeled. Both of these effects are very common in gas-turbine applications of total temperature probes. This Thesis will present a fundamental study analyzing the impact that freestream flow angle and a probe’s mount have on a total temperature probe’s measurement error. The influence of conduction and convection heat transfer was studied experimentally for numerous probe geometries, and the impacts of a mounting strut and freestream flow angle were analyzed. A low-order method was developed to predict conduction error and aerodynamic error for total temperature probes in offangle conditions with the presence of mount interference. The developed low-order method was shown to accurately capture the effects of a mounting strut, varying probe geometry, and varying flow angle. Additionally, the low-order method was validated against experimental and 3D, CFD/CHT results.
Lopera, Javier. "Aerodynamic Control of Slender Bodies from Low to High Angles of Attack through Flow Manipulation". Connect to Online Resource-OhioLINK, 2007. http://www.ohiolink.edu/etd/view.cgi?acc_num=toledo1177504352.
Texto completoHammer, Patrick Richard. "A Discrete Vortex Method Application to Low Reynolds Number Aerodynamic Flows". University of Dayton / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1311792450.
Texto completoLibros sobre el tema "Aerodynamic angle"
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Actuator and aerodynamic modeling for high-angle-of-attack aeroservoelasticity. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. High angle-of-attack aerodynamic characteristics of crescent and elliptic wings. Davis, CA: University of California, Dept. of Mechanical Engineering, Division of Aeronautical Science and Engineering, 1989.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. High angle-of-attack aerodynamic characteristics of crescent and elliptic wings. Davis, CA: University of California, Dept. of Mechanical Engineering, Division of Aeronautical Science and Engineering, 1989.
Buscar texto completoMatsuo, N. Aerodynamic characteristics of general aviation at high angle of attack with the propeller slipstream. Washington DC: National Aeronautics and Space Administration, 1987.
Buscar texto completoKlein, Vladislav. Aerodynamic parameters of High-Angle-of-Attack Research Vehicle (HARV) estimated from flight data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Buscar texto completoKlein, Vladislav. Aerodynamic parameters of high-angle-of-attack research vehicle (Harv) estimated from flight data. Hampton, Va: National Aeronautics and Space Administration, 1990.
Buscar texto completoCenter, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Buscar texto completoCenter, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Buscar texto completoCenter, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Buscar texto completoCenter, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Buscar texto completoCapítulos de libros sobre el tema "Aerodynamic angle"
Hage, W., D. W. Bechert y M. Bruse. "Yaw Angle Effects on Optimized Riblets". En Aerodynamic Drag Reduction Technologies, 278–85. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-540-45359-8_29.
Texto completoNakamura, Y., Y. Nakajima y W. Jia. "Aerodynamic Characteristics of Thick Delta Wing". En Fluid Dynamics of High Angle of Attack, 375–82. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-52460-8_26.
Texto completoMorishita, E., H. Koyama, T. Kitamori y Y. Aihara. "Unsteady Aerodynamic Characteristics of Deformable Airfoil". En Fluid Dynamics of High Angle of Attack, 91–105. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-52460-8_5.
Texto completoDriss, Zied, Olfa Mlayeh, Dorra Driss, Makram Maaloul y Mohamed Salah Abid. "Incidence Angle Effect on the Aerodynamic Structure of an Incurved Savonius Wind Rotor". En Applied Condition Monitoring, 101–10. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-14532-7_11.
Texto completoFrikha, Sobhi, Zied Driss, Hedi Kchaou y Mohamed Salah Abid. "Study of the Incidence Angle Effect on a Savonius Wind Rotor Aerodynamic Structure". En CFD Techniques and Energy Applications, 161–77. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-70950-5_8.
Texto completoDalbanjan, Manjunath S. y Niranjan Sarangi. "Sensitivity Study of Stagger Angle on the Aerodynamic Performance of Transonic Axial Flow Compressors". En Proceedings of the National Aerospace Propulsion Conference, 3–14. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2378-4_1.
Texto completoWang, Yangwei, Jian Wang y Jun Zhang. "Effects of Wind Rotor Tilt Angle on Aerodynamic Power of Wind Turbine under Typical Periodic Disturbances". En Advances in Mechanism and Machine Science, 3459–68. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-20131-9_341.
Texto completoKargarnovin, Mohammad H. y Mohammad H. Sayrarfie. "Vibrational Response vs. Change of Trailing Sweep Angle, Tip Angle and Wing’s Thickness of a Small Wing Under Aerodynamic and Aeroelastic Forces in Super Sonic Range". En Computational Mechanics ’95, 1047–52. Berlin, Heidelberg: Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-79654-8_171.
Texto completoRom, Josef. "Introduction". En High Angle of Attack Aerodynamics, 1–7. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2824-0_1.
Texto completoRom, Josef. "Description of Flows at High Angles of Attack". En High Angle of Attack Aerodynamics, 8–61. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2824-0_2.
Texto completoActas de conferencias sobre el tema "Aerodynamic angle"
Didyk, Z. V. y V. A. Apostolyuk. "Whole angle approximations of aerodynamic coefficients". En 2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC). IEEE, 2012. http://dx.doi.org/10.1109/msnmc.2012.6475107.
Texto completoNELSON, ROBERT. "Visualization techniques for studying high angle of attack separatedvortical flows". En 15th Aerodynamic Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2025.
Texto completoJouannet, Christopher y Petter Krus. "Modelling of High Angle of Attack Aerodynamic". En 25th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-4295.
Texto completoAbney, Eric y Melissa McDaniel. "High Angle of Attack Aerodynamic Predictions Using Missile Datcom". En 23rd AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-5086.
Texto completoAbdel-Salam, T., S. Tiwari y T. Mohieldin. "Effects of ramp swept angle in supersonic mixing". En 21st Aerodynamic Measurement Technology and Ground Testing Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-2377.
Texto completoMcCrink, Matthew y James W. Gregory. "Aerodynamic Parameter Estimation for Derived Angle-of-Attack Systems". En AIAA Atmospheric Flight Mechanics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4061.
Texto completoKumar, Rajeev y Sergey Shkarayev. "Effects of Yaw Angle on Aerodynamic Response in Locusts". En 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-417.
Texto completoBao, Haitao, Cheng Wang y Yonghai Wu. "Effects of Rear Window Angle on Car Aerodynamic Characteristics". En 2020 3rd World Conference on Mechanical Engineering and Intelligent Manufacturing (WCMEIM). IEEE, 2020. http://dx.doi.org/10.1109/wcmeim52463.2020.00141.
Texto completoXuechang, Zhu, Yu Xiaojing y Hong Yan. "Aerodynamic Characteristics of Fairing Separation at Initial Opening Angle". En 1st International Conference on Mechanical Engineering and Material Science). Paris, France: Atlantis Press, 2012. http://dx.doi.org/10.2991/mems.2012.160.
Texto completoJouannet, Christopher y Petter Krus. "Modelling of High Angle of Attack Aerodynamic, a State-Space Approach". En 24th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3845.
Texto completoInformes sobre el tema "Aerodynamic angle"
Bihrle, W., Barnhart Jr., Dickes B. y E. Static and Rotational Aerodynamic Data from O deg to 90 deg Angle of Attack for a Series of Basic and Altered Forebody Shapes. Fort Belvoir, VA: Defense Technical Information Center, septiembre de 1989. http://dx.doi.org/10.21236/ada216582.
Texto completoMcInville, Roy M. y Frank G. Moore. A New Method for Calculating Wing Along Aerodynamics to Angle of Attack 180 deg. Fort Belvoir, VA: Defense Technical Information Center, marzo de 1994. http://dx.doi.org/10.21236/ada277965.
Texto completoBowersox, Rodney D. y Huaiguo Fan. Investigation of Combined Low-Angled Jets and Variable Wall Geometry for Hypersonic Aerodynamic Control. Fort Belvoir, VA: Defense Technical Information Center, noviembre de 2000. http://dx.doi.org/10.21236/ada384726.
Texto completoAerodynamic Development of the GAC ENO.146 Concept. SAE International, septiembre de 2021. http://dx.doi.org/10.4271/2021-01-5093.
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