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Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows 2015 Edition
Contributor(s): Ayton, Lorna (Author)
ISBN: 3319199587     ISBN-13: 9783319199580
Publisher: Springer
OUR PRICE:   $104.49  
Product Type: Hardcover - Other Formats
Published: June 2015
Qty:
Additional Information
BISAC Categories:
- Science | Acoustics & Sound
- Technology & Engineering | Acoustics & Sound
- Science | Physics - Mathematical & Computational
Dewey: 003.3
Series: Springer Theses
Physical Information: 0.5" H x 6.14" W x 9.21" (1.02 lbs) 178 pages
 
Descriptions, Reviews, Etc.
Publisher Description:
This thesis investigates the sound generated by solid bodies in steady subsonic flows with unsteady perturbations, as is typically used when determining the noise generated by turbulent interactions. The focus is predominantly on modelling the sound generated by blades within an aircraft engine, and the solutions are presented as asymptotic approximations. Key analytical techniques, such as the Wiener-Hopf method, and the matched asymptotic expansion method are clearly detailed. The results allow for the effect of variations in the steady flow or blade shape on the noise generated to be analysed much faster than when solving the problem numerically or considering it experimentally.

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