Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows

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...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής
Κύριος συγγραφέας: Ayton, Lorna (Συγγραφέας)
Συγγραφή απο Οργανισμό/Αρχή: SpringerLink (Online service)
Μορφή: Ηλεκτρονική πηγή Ηλ. βιβλίο
Γλώσσα:English
Έκδοση: Cham : Springer International Publishing : Imprint: Springer, 2015.
Σειρά:Springer Theses, Recognizing Outstanding Ph.D. Research,
Θέματα:
Διαθέσιμο Online:Full Text via HEAL-Link
LEADER 02835nam a22004935i 4500
001 978-3-319-19959-7
003 DE-He213
005 20151204141931.0
007 cr nn 008mamaa
008 150615s2015 gw | s |||| 0|eng d
020 |a 9783319199597  |9 978-3-319-19959-7 
024 7 |a 10.1007/978-3-319-19959-7  |2 doi 
040 |d GrThAP 
050 4 |a QC221-246 
072 7 |a PHDS  |2 bicssc 
072 7 |a SCI001000  |2 bisacsh 
082 0 4 |a 534  |2 23 
100 1 |a Ayton, Lorna.  |e author. 
245 1 0 |a Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows  |h [electronic resource] /  |c by Lorna Ayton. 
264 1 |a Cham :  |b Springer International Publishing :  |b Imprint: Springer,  |c 2015. 
300 |a XXI, 178 p. 48 illus., 6 illus. in color.  |b online resource. 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
347 |a text file  |b PDF  |2 rda 
490 1 |a Springer Theses, Recognizing Outstanding Ph.D. Research,  |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 Physics. 
650 0 |a Mathematical models. 
650 0 |a Acoustics. 
650 0 |a Acoustical engineering. 
650 1 4 |a Physics. 
650 2 4 |a Acoustics. 
650 2 4 |a Engineering Acoustics. 
650 2 4 |a Mathematical Methods in Physics. 
650 2 4 |a Mathematical Modeling and Industrial Mathematics. 
710 2 |a SpringerLink (Online service) 
773 0 |t Springer eBooks 
776 0 8 |i Printed edition:  |z 9783319199580 
830 0 |a Springer Theses, Recognizing Outstanding Ph.D. Research,  |x 2190-5053 
856 4 0 |u http://dx.doi.org/10.1007/978-3-319-19959-7  |z Full Text via HEAL-Link 
912 |a ZDB-2-PHA 
950 |a Physics and Astronomy (Springer-11651)