Littérature scientifique sur le sujet « Aerodynamic angle »
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Articles de revues sur le sujet "Aerodynamic angle"
Tripathi, Manish, Mahesh M. Sucheendran et 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, no 3 (5 septembre 2019) : 537–62. http://dx.doi.org/10.1177/0954410019872349.
Texte intégralSun, Xiao-Ying, Tian-E. Li, Guo-Chang Lin et 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, no 5 (2 août 2017) : 902–21. http://dx.doi.org/10.1177/0954410017723358.
Texte intégralTaiming, Huang, Zhuang Xiaodong, Wan Zhongmin et 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, no 8 (7 février 2020) : 2216–27. http://dx.doi.org/10.1177/0954407019893849.
Texte intégralBaigang, Mi, et Yu Jingyi. « An Improved Nonlinear Aerodynamic Derivative Model of Aircraft at High Angles of Attack ». International Journal of Aerospace Engineering 2021 (8 septembre 2021) : 1–12. http://dx.doi.org/10.1155/2021/5815167.
Texte intégralXiang, Jinwu, Kai Liu, Daochun Li, Chunxiao Cheng et Enlai Sha. « Unsteady aerodynamic characteristics of a morphing wing ». Aircraft Engineering and Aerospace Technology 91, no 1 (7 janvier 2018) : 1–9. http://dx.doi.org/10.1108/aeat-04-2017-0101.
Texte intégralHu, Haode, et Dongli Ma. « Airfoil Aerodynamics in Proximity to Wavy Ground for a Wide Range of Angles of Attack ». Applied Sciences 10, no 19 (27 septembre 2020) : 6773. http://dx.doi.org/10.3390/app10196773.
Texte intégralZhang, Yanqi, et Zhaoming Zhang. « Unsteady Aerodynamic Characteristics of Antenna Rotating in Different Elevation Angles ». International Journal of Antennas and Propagation 2021 (26 juillet 2021) : 1–16. http://dx.doi.org/10.1155/2021/5503330.
Texte intégralWang, Xu, Yuanhao Qian, Zengshun Chen, Xiao Zhou, Huaqiang Li et Hailin Huang. « Numerical studies on aerodynamics of high-speed railway train subjected to strong crosswind ». Advances in Mechanical Engineering 11, no 11 (novembre 2019) : 168781401988727. http://dx.doi.org/10.1177/1687814019887270.
Texte intégralHUANG, DA, et GENXIN WU. « INVESTIGATION OF SUITABILITY FOR THE LINEAR SUPERPOSITION MODEL ». Modern Physics Letters B 19, no 28n29 (20 décembre 2005) : 1631–34. http://dx.doi.org/10.1142/s0217984905010086.
Texte intégralKang, Chang-kwon, et 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, no 101 (6 décembre 2014) : 20140933. http://dx.doi.org/10.1098/rsif.2014.0933.
Texte intégralThèses sur le sujet "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.
Texte intégralFan, Yigang. « Identification of an Unsteady Aerodynamic Model up to High Angle of Attack Regime ». Diss., Virginia Tech, 1997. http://hdl.handle.net/10919/29830.
Texte intégralPh. 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.
Texte intégralMaster 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.
Texte intégralSor, Wei Lun. « Aerodynamic Validation of Emerging Projectile Configurations ». Thesis, Monterey, California. Naval Postgraduate School, 2012.
Trouver le texte intégralEver-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 et 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.
Texte intégralMohmad, 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.
Texte intégralQuickel, Reuben Alexander. « Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes ». Thesis, Virginia Tech, 2019. http://hdl.handle.net/10919/89952.
Texte intégralMaster 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.
Texte intégralHammer, 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.
Texte intégralLivres sur le sujet "Aerodynamic angle"
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. 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.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. 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.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. 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.
Trouver le texte intégralMatsuo, N. Aerodynamic characteristics of general aviation at high angle of attack with the propeller slipstream. Washington DC : National Aeronautics and Space Administration, 1987.
Trouver le texte intégralKlein, 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.
Trouver le texte intégralKlein, Vladislav. Aerodynamic parameters of high-angle-of-attack research vehicle (Harv) estimated from flight data. Hampton, Va : National Aeronautics and Space Administration, 1990.
Trouver le texte intégralCenter, Ames Research, dir. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1998.
Trouver le texte intégralCenter, Ames Research, dir. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1998.
Trouver le texte intégralCenter, Ames Research, dir. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1998.
Trouver le texte intégralCenter, Ames Research, dir. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1998.
Trouver le texte intégralChapitres de livres sur le sujet "Aerodynamic angle"
Hage, W., D. W. Bechert et M. Bruse. « Yaw Angle Effects on Optimized Riblets ». Dans Aerodynamic Drag Reduction Technologies, 278–85. Berlin, Heidelberg : Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-540-45359-8_29.
Texte intégralNakamura, Y., Y. Nakajima et W. Jia. « Aerodynamic Characteristics of Thick Delta Wing ». Dans 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.
Texte intégralMorishita, E., H. Koyama, T. Kitamori et Y. Aihara. « Unsteady Aerodynamic Characteristics of Deformable Airfoil ». Dans 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.
Texte intégralDriss, Zied, Olfa Mlayeh, Dorra Driss, Makram Maaloul et Mohamed Salah Abid. « Incidence Angle Effect on the Aerodynamic Structure of an Incurved Savonius Wind Rotor ». Dans Applied Condition Monitoring, 101–10. Cham : Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-14532-7_11.
Texte intégralFrikha, Sobhi, Zied Driss, Hedi Kchaou et Mohamed Salah Abid. « Study of the Incidence Angle Effect on a Savonius Wind Rotor Aerodynamic Structure ». Dans CFD Techniques and Energy Applications, 161–77. Cham : Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-70950-5_8.
Texte intégralDalbanjan, Manjunath S., et Niranjan Sarangi. « Sensitivity Study of Stagger Angle on the Aerodynamic Performance of Transonic Axial Flow Compressors ». Dans 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.
Texte intégralWang, Yangwei, Jian Wang et Jun Zhang. « Effects of Wind Rotor Tilt Angle on Aerodynamic Power of Wind Turbine under Typical Periodic Disturbances ». Dans 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.
Texte intégralKargarnovin, Mohammad H., et 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 ». Dans Computational Mechanics ’95, 1047–52. Berlin, Heidelberg : Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-79654-8_171.
Texte intégralRom, Josef. « Introduction ». Dans 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.
Texte intégralRom, Josef. « Description of Flows at High Angles of Attack ». Dans 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.
Texte intégralActes de conférences sur le sujet "Aerodynamic angle"
Didyk, Z. V., et V. A. Apostolyuk. « Whole angle approximations of aerodynamic coefficients ». Dans 2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC). IEEE, 2012. http://dx.doi.org/10.1109/msnmc.2012.6475107.
Texte intégralNELSON, ROBERT. « Visualization techniques for studying high angle of attack separatedvortical flows ». Dans 15th Aerodynamic Testing Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2025.
Texte intégralJouannet, Christopher, et Petter Krus. « Modelling of High Angle of Attack Aerodynamic ». Dans 25th AIAA Applied Aerodynamics Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-4295.
Texte intégralAbney, Eric, et Melissa McDaniel. « High Angle of Attack Aerodynamic Predictions Using Missile Datcom ». Dans 23rd AIAA Applied Aerodynamics Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-5086.
Texte intégralAbdel-Salam, T., S. Tiwari et T. Mohieldin. « Effects of ramp swept angle in supersonic mixing ». Dans 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.
Texte intégralMcCrink, Matthew, et James W. Gregory. « Aerodynamic Parameter Estimation for Derived Angle-of-Attack Systems ». Dans AIAA Atmospheric Flight Mechanics Conference. Reston, Virginia : American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4061.
Texte intégralKumar, Rajeev, et Sergey Shkarayev. « Effects of Yaw Angle on Aerodynamic Response in Locusts ». Dans 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.
Texte intégralBao, Haitao, Cheng Wang et Yonghai Wu. « Effects of Rear Window Angle on Car Aerodynamic Characteristics ». Dans 2020 3rd World Conference on Mechanical Engineering and Intelligent Manufacturing (WCMEIM). IEEE, 2020. http://dx.doi.org/10.1109/wcmeim52463.2020.00141.
Texte intégralXuechang, Zhu, Yu Xiaojing et Hong Yan. « Aerodynamic Characteristics of Fairing Separation at Initial Opening Angle ». Dans 1st International Conference on Mechanical Engineering and Material Science). Paris, France : Atlantis Press, 2012. http://dx.doi.org/10.2991/mems.2012.160.
Texte intégralJouannet, Christopher, et Petter Krus. « Modelling of High Angle of Attack Aerodynamic, a State-Space Approach ». Dans 24th AIAA Applied Aerodynamics Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3845.
Texte intégralRapports d'organisations sur le sujet "Aerodynamic angle"
Bihrle, W., Barnhart Jr., Dickes B. et 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, septembre 1989. http://dx.doi.org/10.21236/ada216582.
Texte intégralMcInville, Roy M., et Frank G. Moore. A New Method for Calculating Wing Along Aerodynamics to Angle of Attack 180 deg. Fort Belvoir, VA : Defense Technical Information Center, mars 1994. http://dx.doi.org/10.21236/ada277965.
Texte intégralBowersox, Rodney D., et Huaiguo Fan. Investigation of Combined Low-Angled Jets and Variable Wall Geometry for Hypersonic Aerodynamic Control. Fort Belvoir, VA : Defense Technical Information Center, novembre 2000. http://dx.doi.org/10.21236/ada384726.
Texte intégralAerodynamic Development of the GAC ENO.146 Concept. SAE International, septembre 2021. http://dx.doi.org/10.4271/2021-01-5093.
Texte intégral