Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows / Springer Theses (PDF)

Name: Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows / Springer Theses
Brand: Springer-Verlag GmbH
SKU: 69960261
Price: 98.99 EUR
Availability: OnlineOnly

(Sprache: Englisch)

Autor: Lorna Ayton

Schreiben Sie einen Kommentar zu "Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows / Springer Theses".

Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows / Springer Theses, Lorna Ayton

Merken

Mehr zum Inhalt Video

eBook (pdf) 98.99 €

Buch (Gebunden) 109.99 €

sofort als Download lieferbar

Bestellnummer: 69960261

Printausgabe 109.99 €

eBook (pdf) -10% 98.99 €

Download bestellen

Verschenken

Lastschrift, Kreditkarte, Paypal, Rechnung
Kostenloser tolino webreader

Produktdetails

Produktbeschreibung
eBook Hilfe
Biblio. Angaben / Produktdetails

Produktinformationen zu „Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows / Springer Theses (PDF)“

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.