Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows /

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Bibliographic Details
Author / Creator:	Ayton, Lorna, author.
Imprint:	Cham : Springer, 2015. ©2015
Description:	1 online resource : illustrations (chiefly color).
Language:	English
Series:	Springer theses, 2190-5061 Springer theses.
Subject:	Aerodynamic noise -- Mathematical models. Aerofoils -- Research. Unsteady flow (Aerodynamics) -- Mathematical models. SCIENCE -- Mechanics -- Aerodynamics. TECHNOLOGY & ENGINEERING -- Aeronautics & Astronautics. TRANSPORTATION -- Aviation -- General. Aerodynamic noise -- Mathematical models. Aerofoils -- Research. Unsteady flow (Aerodynamics) -- Mathematical models. Electronic books.
Format:	E-Resource Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11094739

Hidden Bibliographic Details
ISBN:	9783319199597 3319199595 3319199587 9783319199580 9783319199580
Digital file characteristics:	text file PDF
Notes:	"Doctoral thesis accepted by the University of Cambridge, UK." Includes bibliographical references. Online resource; title from PDF title page (Ebsco, viewed June 22, 2015).
Summary:	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.
Other form:	Printed edition: 9783319199580
Standard no.:	10.1007/978-3-319-19959-7

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