Titlebook: Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows; Lorna Ayton Book 2015 Springer International Pu

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書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows影響因子(影響力)




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows影響因子(影響力)學科排名




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows網(wǎng)絡公開度




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows網(wǎng)絡公開度學科排名




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows被引頻次




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows被引頻次學科排名




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows年度引用




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows年度引用學科排名




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows讀者反饋




書目名稱Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows讀者反饋學科排名

Dictation

2190-5053 s with realistic geometries.Provides results for high-frequeThis 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

放氣

得意人

Concluding Remarks and Further Work,bsonic, uniform and shear flows; and sound-aerofoil interaction in steady, subsonic uniform flow. To find these solutions we had to separate the solution domain into various asymptotic regions wherein different behaviour dominated the production of sound. The regions were matched using Van Dyke’s matching rule.

syncope

bioavailability

Foundations of GTK+ Development incident gust is high, ., and the thickness and camber angle are small, .. We again impose the preferred scaling ., and use matched asymptotic expansions to split the problem into similar regions as described for the sound-aerofoil interaction problem; these regions can be seen in Fig.?..

樣式

High-Frequency Sound Generated by Gust-Aerofoil Interaction in Subsonic Uniform Flow, incident gust is high, ., and the thickness and camber angle are small, .. We again impose the preferred scaling ., and use matched asymptotic expansions to split the problem into similar regions as described for the sound-aerofoil interaction problem; these regions can be seen in Fig.?..

寬度

curriculum

Introduction,y noise generating features. Early and modern turbofans are compared, showing a very notable reduction in jet noise, but the remaining contributions have not been reduced as significantly. Figure?. shows a typical turboengine found on a large passenger aircraft, and Fig.?. illustrates the important

高興一回

2190-5053 eady flow or blade shape on the noise generated to be analysed much faster than when solving the problem numerically or considering it experimentally.978-3-319-38702-4978-3-319-19959-7Series ISSN 2190-5053 Series E-ISSN 2190-5061