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Ayton, Lorna.

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

Record Type:	Language materials, printed : Monograph/item
Title/Author:	Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows/ by Lorna Ayton.
Author:	Ayton, Lorna.
Published:	Cham :Springer International Publishing : : 2015.,
Description:	xxi, 178 p. :ill., digital ;24 cm.
[NT 15003449]:	High-Frequency Sound Generated by Sound-Aerofoil Interaction in Subsonic Uniform Flow -- High-Frequency Sound Generated by Gust-Aerofoil Interaction in Subsonic Uniform Flow -- High-Frequency Sound Generated by Gust-Aerofoil Interaction in Subsonic Shear Flow -- Leading-Edge Stagnation-Point Noise Generated by Turbulence in Subsonic Uniform Flow -- Concluding Remarks and Further Work.
Contained By:	Springer eBooks
Subject:	Aerodynamic noise - Mathematical models. -
Online resource:	http://dx.doi.org/10.1007/978-3-319-19959-7
ISBN:	9783319199597 (electronic bk.)

Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows
Ayton, Lorna.

Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows[electronic resource] /by Lorna Ayton. - Cham :Springer International Publishing :2015. - xxi, 178 p. :ill., digital ;24 cm. - Springer theses,2190-5053. - Springer theses..

High-Frequency Sound Generated by Sound-Aerofoil Interaction in Subsonic Uniform Flow -- High-Frequency Sound Generated by Gust-Aerofoil Interaction in Subsonic Uniform Flow -- High-Frequency Sound Generated by Gust-Aerofoil Interaction in Subsonic Shear Flow -- Leading-Edge Stagnation-Point Noise Generated by Turbulence in Subsonic Uniform Flow -- Concluding Remarks and Further Work.

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.

ISBN: 9783319199597 (electronic bk.)

Standard No.: 10.1007/978-3-319-19959-7doiSubjects--Topical Terms:

2156987
Aerodynamic noise
--Mathematical models.

LC Class. No.: TL574.N6

Dewey Class. No.: 629.1323

Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows
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245 1 0 $a Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows $h [electronic resource] / $c by Lorna Ayton.
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490 1 $a Springer theses, $x 2190-5053
505 0 $a High-Frequency Sound Generated by Sound-Aerofoil Interaction in Subsonic Uniform Flow -- High-Frequency Sound Generated by Gust-Aerofoil Interaction in Subsonic Uniform Flow -- High-Frequency Sound Generated by Gust-Aerofoil Interaction in Subsonic Shear Flow -- Leading-Edge Stagnation-Point Noise Generated by Turbulence in Subsonic Uniform Flow -- Concluding Remarks and Further Work.
520 $a 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.
650 0 $a Aerodynamic noise $x Mathematical models. $3 2156987
650 0 $a Aerofoils $x Research. $3 2156988
650 0 $a Unsteady flow (Aerodynamics) $x Mathematical models. $3 2156989
650 1 4 $a Physics. $3 516296
650 2 4 $a Acoustics. $3 879105
650 2 4 $a Engineering Acoustics. $3 1533220
650 2 4 $a Mathematical Methods in Physics. $3 890898
650 2 4 $a Mathematical Modeling and Industrial Mathematics. $3 891089
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830 0 $a Springer theses. $3 1314442
856 4 0 $u http://dx.doi.org/10.1007/978-3-319-19959-7
950 $a Physics and Astronomy (Springer-11651)