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...
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| Định dạng: | Sách |
| Ngôn ngữ: | English |
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Springer
2016
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| Truy cập trực tuyến: | https://scholar.dlu.edu.vn/thuvienso/handle/DLU123456789/59829 |
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oai:scholar.dlu.edu.vn:DLU123456789-598292023-11-11T06:53:21Z Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows Ayton, Lorna Mathematical models Unsteady flow Research Aerofoils Mathematical models Aerodynamic noise 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. 2016-03-15T07:17:36Z 2016-03-15T07:17:36Z 2015 Book 978-3-319-19959-7 978-3-319-19958-0 https://scholar.dlu.edu.vn/thuvienso/handle/DLU123456789/59829 en application/pdf Springer |
| institution |
Thư viện Trường Đại học Đà Lạt |
| collection |
Thư viện số |
| language |
English |
| topic |
Mathematical models Unsteady flow Research Aerofoils Mathematical models Aerodynamic noise |
| spellingShingle |
Mathematical models Unsteady flow Research Aerofoils Mathematical models Aerodynamic noise Ayton, Lorna Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows |
| description |
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. |
| format |
Book |
| author |
Ayton, Lorna |
| author_facet |
Ayton, Lorna |
| author_sort |
Ayton, Lorna |
| title |
Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows |
| title_short |
Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows |
| title_full |
Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows |
| title_fullStr |
Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows |
| title_full_unstemmed |
Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows |
| title_sort |
asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows |
| publisher |
Springer |
| publishDate |
2016 |
| url |
https://scholar.dlu.edu.vn/thuvienso/handle/DLU123456789/59829 |
| _version_ |
1819770178281406464 |