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Статті в журналах з теми "Aerofoil Noise"
Laratro, Alex, Maziar Arjomandi, Benjamin Cazzolato, and Richard Kelso. "Self-noise of NACA 0012 and NACA 0021 aerofoils at the onset of stall." International Journal of Aeroacoustics 16, no. 3 (April 2017): 181–95. http://dx.doi.org/10.1177/1475472x17709929.
Повний текст джерелаChaitanya, P., P. Joseph, S. Narayanan, C. Vanderwel, J. Turner, J. W. Kim, and B. Ganapathisubramani. "Performance and mechanism of sinusoidal leading edge serrations for the reduction of turbulence–aerofoil interaction noise." Journal of Fluid Mechanics 818 (April 4, 2017): 435–64. http://dx.doi.org/10.1017/jfm.2017.141.
Повний текст джерелаAyton, Lorna J., and Paruchuri Chaitanya. "Analytical and experimental investigation into the effects of leading-edge radius on gust–aerofoil interaction noise." Journal of Fluid Mechanics 829 (September 26, 2017): 780–808. http://dx.doi.org/10.1017/jfm.2017.594.
Повний текст джерелаNASH, EMMA C., MARTIN V. LOWSON, and ALAN McALPINE. "Boundary-layer instability noise on aerofoils." Journal of Fluid Mechanics 382 (March 10, 1999): 27–61. http://dx.doi.org/10.1017/s002211209800367x.
Повний текст джерелаAyton, Lorna J., and N. Peake. "On high-frequency noise scattering by aerofoils in flow." Journal of Fluid Mechanics 734 (October 8, 2013): 144–82. http://dx.doi.org/10.1017/jfm.2013.477.
Повний текст джерелаYakhina, Gyuzel, Michel Roger, Stéphane Moreau, Lap Nguyen, and Vladimir Golubev. "Experimental and Analytical Investigation of the Tonal Trailing-Edge Noise Radiated by Low Reynolds Number Aerofoils." Acoustics 2, no. 2 (May 14, 2020): 293–329. http://dx.doi.org/10.3390/acoustics2020018.
Повний текст джерелаHajian, Rozhin, and Justin W. Jaworski. "The steady aerodynamics of aerofoils with porosity gradients." Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences 473, no. 2205 (September 2017): 20170266. http://dx.doi.org/10.1098/rspa.2017.0266.
Повний текст джерелаChaitanya, P., P. Joseph, S. Narayanan, and J. W. Kim. "Aerofoil broadband noise reductions through double-wavelength leading-edge serrations: a new control concept." Journal of Fluid Mechanics 855 (September 14, 2018): 131–51. http://dx.doi.org/10.1017/jfm.2018.620.
Повний текст джерелаSATO, Yukiko, and Hideki ONODERA. "Reduction of aerodynamic noise from windturbine aerofoil." Proceedings of Autumn Conference of Tohoku Branch 2003.39 (2003): 139–40. http://dx.doi.org/10.1299/jsmetohoku.2003.39.139.
Повний текст джерелаPröbsting, S., J. Serpieri, and F. Scarano. "Experimental investigation of aerofoil tonal noise generation." Journal of Fluid Mechanics 747 (April 23, 2014): 656–87. http://dx.doi.org/10.1017/jfm.2014.156.
Повний текст джерелаДисертації з теми "Aerofoil Noise"
Kingan, Michael Joseph. "Aeroacoustic noise produced by an aerofoil." Thesis, University of Canterbury. Mechanical Engineering, 2005. http://hdl.handle.net/10092/6596.
Повний текст джерелаParuchuri, Chaitanya. "Aerofoil geometry effects on turbulence interaction noise." Thesis, University of Southampton, 2017. https://eprints.soton.ac.uk/415884/.
Повний текст джерелаAi, Qing. "Novel morphing structures for aerofoil flow and noise control purposes." Thesis, University of Bristol, 2016. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.720818.
Повний текст джерелаLau, Alex Siu Hong. "High-order computations on aerofoil-gust interaction noise and the effects of wavy leading edges." Thesis, University of Southampton, 2012. https://eprints.soton.ac.uk/355961/.
Повний текст джерелаNash, Emma Clare. "Boundary layer instability noise on aerofoils." Thesis, University of Bristol, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.337698.
Повний текст джерелаFosas, De Pando Miguel Ángel. "Tonal noise generation in flows around aerofoils : a global stability analysis." Palaiseau, Ecole polytechnique, 2012. https://theses.hal.science/tel-00816987.
Повний текст джерелаThe generation of discrete acoustic tones in the compressible flow around an aerofoil is addressed in this thesis by means of nonlinear numerical simulations and global stability analyses. To this end, a nonlinear simulation code featuring a novel technique for gaining access to the linearized direct and adjoint dynamics has been developed and applied to the flow around an aerofoil. The nonlinear simulations confirm the appearance of discrete tones in the acoustic spectrum, and for the chosen flow case, the global stability analyses of the mean-flow dynamics reveal that the linearized operator is stable. However, the flow response to incoming disturbances exhibits important transient growth effects that culminate into the onset of aeroacoustic feedback loops, involving instability process on the suction- and pressure-surface boundary-layers together with their cross interaction by acoustic radiation at the trailing edge. The features of the aeroacoustic feedback loops and the appearance of discrete tones are then related to the features of the least stable modes in the global spectrum: on the one hand, the spatial structure of the direct modes display the growth of hydrodynamic instabilities on the suction surface and the near wake; on the other hand, the associated adjoint modes display increased receptivity of the flow on the pressure surface. Finally, the analysis of the wavemaker region highlights, in agreement with previous experimental investigations, the sensitivity of the flow to the pressure-surface boundary layer
Ferret, Bernard. "Etude expérimentale de l'intéraction entre un tourbillon isolé et un profil d'aile." Poitiers, 1988. http://www.theses.fr/1988POIT2317.
Повний текст джерелаMYERS, MATTHEW RONALD. "EFFECT OF AIRFOIL MEAN LOADING ON HIGH-FREQUENCY GUST INTERACTION NOISE (AEROACOUSTICS, FAN, TURBOMACHINERY)." Diss., The University of Arizona, 1987. http://hdl.handle.net/10150/184032.
Повний текст джерелаSchumacher, Karn Lee. "Low Reynolds Number Two- and Three-Dimensional Cavity Flows and the Effect of a Cavity on Airfoil Tonal Noise." Thesis, 2020. https://hdl.handle.net/2440/135369.
Повний текст джерелаThesis (Ph.D.) -- University of Adelaide, School of Mechanical Engineering, 2020
Книги з теми "Aerofoil Noise"
Brooks, Thomas F. Airfoil self-noise and prediction. Hampton, Va: Langley Research Center, 1989.
Знайти повний текст джерелаBrooks, Thomas F. Airfoil self-noise and prediction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаBrooks, Thomas F. Airfoil self-noise and prediction. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаBrooks, Thomas F. Airfoil self-noise and prediction. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаBrooks, Thomas F. Airfoil self-noise and prediction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаStuart, Pope D., Marcolini Michael A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, eds. Airfoil self-noise and prediction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаStuart, Pope D., Marcolini Michael A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, eds. Airfoil self-noise and prediction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаAirfoil self-noise and prediction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Знайти повний текст джерелаЧастини книг з теми "Aerofoil Noise"
Ayton, Lorna. "Leading-Edge Stagnation-Point Noise Generated by Turbulence in Subsonic Uniform Flow." In Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows, 145–74. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-19959-7_5.
Повний текст джерелаPrasad Maddula, Satya, Vasishta Bhargava Nukala, Swamy Naidu Neigapula Venkata, Chinmaya Prasad Padhy, and Rahul Samala. "Trailing Edge Bluntness Noise Characterization for Horizontal Axis Wind Turbines [HAWT] Blades." In Acoustic Emission - New Perspectives and Applications. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.99880.
Повний текст джерелаТези доповідей конференцій з теми "Aerofoil Noise"
Woodhead, Philip C., Tze Pei Chong, Phillip Joseph, Jan G. Wissink, and Paruchuri Chaitanya. "Frequency-Targetable Aerofoil Self-Noise Reduction." In AIAA AVIATION 2021 FORUM. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-2229.
Повний текст джерелаParuchuri, Chaitanya, James R. Gill, Narayanan Subramanian, Phillip Joseph, Christina Vanderwel, Xin Zhang, and Bharathram Ganapathisubramani. "Aerofoil geometry effects on turbulence interaction noise." In 21st AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-2830.
Повний текст джерелаLeung, Ronnie, Chaitanya C. Paruchuri, and Phillip Joseph. "Effect of aerofoil thickness on trailing edge noise." In 22nd AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-2814.
Повний текст джерелаDeuse, Mathieu, and Richard D. Sandberg. "Parametric study of multiple aerofoil self-noise sources using direct noise computation." In 25th AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-2681.
Повний текст джерелаDeuse, Mathieu, and Richard D. Sandberg. "Correction: Parametric study of multiple aerofoil self-noise sources using direct noise computation." In 25th AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-2681.c1.
Повний текст джерелаVathylakis, Alexandros, Chaitanya C. Paruchuri, Tze Pei Chong, and Phillip Joseph. "Sensitivity of aerofoil self-noise reductions to serration flap angles." In 22nd AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-2837.
Повний текст джерелаAyton, Lorna J., Matthew Colbrook, Thomas F. Geyer, Paruchuri Chaitanya, and Ennes Sarradj. "Modelling chordwise-varying porosity to reduce aerofoil-turbulence interaction noise." In AIAA AVIATION 2021 FORUM. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-2190.
Повний текст джерелаDe Gennaro, Michele, Andreas Hueppe, Helmut Kuehnelt, Manfred Kaltenbacher, Theodore E. Simos, George Psihoyios, Ch Tsitouras, and Zacharias Anastassi. "Numerical Prediction of Laminar Instability Noise for NACA 0012 Aerofoil." In NUMERICAL ANALYSIS AND APPLIED MATHEMATICS ICNAAM 2011: International Conference on Numerical Analysis and Applied Mathematics. AIP, 2011. http://dx.doi.org/10.1063/1.3636675.
Повний текст джерелаLacagnina, Giovanni, Seyed Mohammad Hasheminejad, Chaitanya C. Paruchuri, Phillip Joseph, Tze Pei Chong, and Oksana Stalnov. "Leading edge serrations for the reduction of aerofoil separation self-noise." In 23rd AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4169.
Повний текст джерелаChong, Tze Pei, Till Biedermann, Oliver Koster, and Seyed Mohammad Hasheminejad. "On the Effect of Leading Edge Serrations on Aerofoil Noise Production." In 2018 AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-3289.
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