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Titlebook: Noise Sources in Turbulent Shear Flows: Fundamentals and Applications; Roberto Camussi Book 2013 CISM,Udine 2013 Airfoil Noise.Boundary La

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21#
發(fā)表于 2025-3-25 06:08:41 | 只看該作者
Roberto CamussiContains both fundamental concepts and applications.State-of-the-art results in the fields of jet noise, noise source identification, boundary layer noise.Includes many practical examples and referenc
22#
發(fā)表于 2025-3-25 11:02:28 | 只看該作者
0254-1971 ry layer noise.Includes many practical examples and referencThe articles in this volume present the state-of-the-art in noise prediction, modeling and measurement. The articles are partially based on class notes provided during the course `Noise sources in turbulent shear flows‘, given at CISM on Ap
23#
發(fā)表于 2025-3-25 15:24:29 | 只看該作者
24#
發(fā)表于 2025-3-25 19:39:07 | 只看該作者
Book 2013s provided during the course `Noise sources in turbulent shear flows‘, given at CISM on April 2011. The first part contains general concepts of aero acoustics, including vortex sound theory and acoustic analogies, in the second part particular emphasis is put into arguments of interest for engineers
25#
發(fā)表于 2025-3-25 20:32:32 | 只看該作者
Jet Noiseng explanations of many observed phenomena. The ability of the different approaches to predict jet noise is assessed. Both subsonic and supersonic jets are considered. Finally, recent prediction methods and experimental observations are described.
26#
發(fā)表于 2025-3-26 02:20:50 | 只看該作者
Analysis techniques for aeroacoustics: noise source identificationure of a fluid flow, and perhaps with phenomenological explanations . our observation of that structure: .. Such kinematic descriptions will very often be with regard to some observable; in aeroacoustics that observable is the radiated sound field: ..
27#
發(fā)表于 2025-3-26 05:50:57 | 只看該作者
Introduction to Aeroacoustics and Self-Sustained Oscillations of Internal Flows from the point of view of a listener immerged in a uniform stagnant fluid. The concept of monopole, dipole and quadrupole are introduced. The scaling of the sound power generated by a subsonic free jet is explained, providing an example of the use of the integral formulation of the analogy. The inf
28#
發(fā)表于 2025-3-26 11:36:15 | 只看該作者
29#
發(fā)表于 2025-3-26 14:38:46 | 只看該作者
Jet Noisew of experimental observations is provided. Only single axisymmetric jets are considered. Then a historical review of theoretical contributions to jet noise understanding and prediction is provided. The emphasis is on both the assumptions and shortcomings of the approaches, in addition to their succ
30#
發(fā)表于 2025-3-26 19:12:28 | 只看該作者
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