Noise Sources in Turbulent Shear Flows: Fundamentals and Applications [electronic resource] /edited by Roberto Camussi.
by Camussi, Roberto [editor.]; SpringerLink (Online service).
Material type:
Item type | Current location | Call number | Status | Date due | Barcode |
---|---|---|---|---|---|
MAIN LIBRARY | TA357-359 (Browse shelf) | Available |
Browsing MAIN LIBRARY Shelves Close shelf browser
RD592.5-596 Minimally Invasive Spinal Deformity Surgery | QD431-431.7 Homocysteine in Protein Structure/Function and Human Disease | RD592.5-596 Brain Edema XV | TA357-359 Noise Sources in Turbulent Shear Flows: Fundamentals and Applications | TJ210.2-211.495 Rob / Arch 2012 | RD592.5-596 Stereotactic and Functional Neurosurgery | TA1-2040 Water Supply Network District Metering |
Fundamentals: Introduction to aero acoustics and self-sustained oscillations of internal flows -- Sound radiation by moving surfaces and the Greens functions techniques -- Applications: Jet noise -- Analysis techniques for aero acoustics: noise source identification -- Broadband noise from lifting surfaces: analytical modeling and experimental validation -- Boundary layer noise: generation mechanisms -- Interior noise radiation and control.
The 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 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 and relevant for aircraft design: jet noise, airfoil broadband noise, boundary layer noise (including interior noise and its control) and the concept of noise sources, their theoretical modeling and identification in turbulent lows. All these arguments are treated extensively with the inclusion of many practical examples and references to engineering applications.
There are no comments for this item.