Theoretical and Computational Aerodynamics:
Aerodynamics has seen many developments due to the growth of scientific computing, which has caused the design cycle time of aerospace vehicles to be heavily reduced. Today computational aerodynamics appears in the preliminary step of a new design, relegating costly, time-consuming wind tunnel testi...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Somerset
Wiley
2014
|
| Ausgabe: | 1st ed |
| Schriftenreihe: | Aerospace Series
|
| Schlagworte: | |
| Online-Zugang: | BTU01 |
| Zusammenfassung: | Aerodynamics has seen many developments due to the growth of scientific computing, which has caused the design cycle time of aerospace vehicles to be heavily reduced. Today computational aerodynamics appears in the preliminary step of a new design, relegating costly, time-consuming wind tunnel testing to the final stages of design. Theoretical and Computational Aerodynamics is aimed to be a comprehensive textbook, covering classical aerodynamic theories and recent applications made possible by computational aerodynamics. It starts with a discussion on lift and drag from an overall dynamical approach, and after stating the governing Navier-Stokes equation, covers potential flows and panel method. Low aspect ratio and delta wings (including vortex breakdown) are also discussed in detail, and after introducing boundary layer theory, computational aerodynamics is covered for DNS and LES. Other topics covered are on flow transition to analyse NLF airfoils, bypass transition, streamwise and cross-flow instability over swept wings, viscous transonic flow over airfoils, low Reynolds number aerodynamics, high lift devices and flow control. Key features: Blends classical theories of incompressible aerodynamics to panel methods Covers lifting surface theories and low aspect ratio wing and wing-body aerodynamics Presents computational aerodynamics from first principles for incompressible and compressible flows Covers unsteady and low Reynolds number aerodynamics Includes an up-to-date account of DNS of airfoil aerodynamics including flow transition for NLF airfoils Contains chapter problems and illustrative examples Accompanied by a website hosting problems and a solution manual Theoretical and Computational Aerodynamics is an ideal textbook for undergraduate and graduate students, and is also aimed to be a useful resource book on aerodynamics for |
| Beschreibung: | Description based on publisher supplied metadata and other sources |
| Beschreibung: | 1 online resource (519 pages) |
| ISBN: | 9781118787540 9781118787595 |
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| 520 | |a Aerodynamics has seen many developments due to the growth of scientific computing, which has caused the design cycle time of aerospace vehicles to be heavily reduced. Today computational aerodynamics appears in the preliminary step of a new design, relegating costly, time-consuming wind tunnel testing to the final stages of design. Theoretical and Computational Aerodynamics is aimed to be a comprehensive textbook, covering classical aerodynamic theories and recent applications made possible by computational aerodynamics. It starts with a discussion on lift and drag from an overall dynamical approach, and after stating the governing Navier-Stokes equation, covers potential flows and panel method. Low aspect ratio and delta wings (including vortex breakdown) are also discussed in detail, and after introducing boundary layer theory, computational aerodynamics is covered for DNS and LES. Other topics covered are on flow transition to analyse NLF airfoils, bypass transition, streamwise and cross-flow instability over swept wings, viscous transonic flow over airfoils, low Reynolds number aerodynamics, high lift devices and flow control. Key features: Blends classical theories of incompressible aerodynamics to panel methods Covers lifting surface theories and low aspect ratio wing and wing-body aerodynamics Presents computational aerodynamics from first principles for incompressible and compressible flows Covers unsteady and low Reynolds number aerodynamics Includes an up-to-date account of DNS of airfoil aerodynamics including flow transition for NLF airfoils Contains chapter problems and illustrative examples Accompanied by a website hosting problems and a solution manual Theoretical and Computational Aerodynamics is an ideal textbook for undergraduate and graduate students, and is also aimed to be a useful resource book on aerodynamics for | ||
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Datensatz im Suchindex
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| author | Sengupta, Tapan K. |
| author_facet | Sengupta, Tapan K. |
| author_role | aut |
| author_sort | Sengupta, Tapan K. |
| author_variant | t k s tk tks |
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| bvnumber | BV043612963 |
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| dewey-full | 629.132/3001 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.132/3001 |
| dewey-search | 629.132/3001 |
| dewey-sort | 3629.132 43001 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| edition | 1st ed |
| format | Electronic eBook |
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| id | DE-604.BV043612963 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T07:30:53Z |
| institution | BVB |
| isbn | 9781118787540 9781118787595 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029027022 |
| oclc_num | 892799668 |
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| physical | 1 online resource (519 pages) |
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| publishDate | 2014 |
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| publisher | Wiley |
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| series2 | Aerospace Series |
| spelling | Sengupta, Tapan K. Verfasser aut Theoretical and Computational Aerodynamics 1st ed Somerset Wiley 2014 © 2014 1 online resource (519 pages) txt rdacontent c rdamedia cr rdacarrier Aerospace Series Description based on publisher supplied metadata and other sources Aerodynamics has seen many developments due to the growth of scientific computing, which has caused the design cycle time of aerospace vehicles to be heavily reduced. Today computational aerodynamics appears in the preliminary step of a new design, relegating costly, time-consuming wind tunnel testing to the final stages of design. Theoretical and Computational Aerodynamics is aimed to be a comprehensive textbook, covering classical aerodynamic theories and recent applications made possible by computational aerodynamics. It starts with a discussion on lift and drag from an overall dynamical approach, and after stating the governing Navier-Stokes equation, covers potential flows and panel method. Low aspect ratio and delta wings (including vortex breakdown) are also discussed in detail, and after introducing boundary layer theory, computational aerodynamics is covered for DNS and LES. Other topics covered are on flow transition to analyse NLF airfoils, bypass transition, streamwise and cross-flow instability over swept wings, viscous transonic flow over airfoils, low Reynolds number aerodynamics, high lift devices and flow control. Key features: Blends classical theories of incompressible aerodynamics to panel methods Covers lifting surface theories and low aspect ratio wing and wing-body aerodynamics Presents computational aerodynamics from first principles for incompressible and compressible flows Covers unsteady and low Reynolds number aerodynamics Includes an up-to-date account of DNS of airfoil aerodynamics including flow transition for NLF airfoils Contains chapter problems and illustrative examples Accompanied by a website hosting problems and a solution manual Theoretical and Computational Aerodynamics is an ideal textbook for undergraduate and graduate students, and is also aimed to be a useful resource book on aerodynamics for Aerodynamics Luft- und Raumfahrtindustrie (DE-588)4048576-6 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Aerodynamik (DE-588)4000589-6 s Luft- und Raumfahrtindustrie (DE-588)4048576-6 s 1\p DE-604 Erscheint auch als Druck-Ausgabe Sengupta, Tapan K . Theoretical and Computational Aerodynamics 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
| spellingShingle | Sengupta, Tapan K. Theoretical and Computational Aerodynamics Aerodynamics Luft- und Raumfahrtindustrie (DE-588)4048576-6 gnd Aerodynamik (DE-588)4000589-6 gnd |
| subject_GND | (DE-588)4048576-6 (DE-588)4000589-6 |
| title | Theoretical and Computational Aerodynamics |
| title_auth | Theoretical and Computational Aerodynamics |
| title_exact_search | Theoretical and Computational Aerodynamics |
| title_full | Theoretical and Computational Aerodynamics |
| title_fullStr | Theoretical and Computational Aerodynamics |
| title_full_unstemmed | Theoretical and Computational Aerodynamics |
| title_short | Theoretical and Computational Aerodynamics |
| title_sort | theoretical and computational aerodynamics |
| topic | Aerodynamics Luft- und Raumfahrtindustrie (DE-588)4048576-6 gnd Aerodynamik (DE-588)4000589-6 gnd |
| topic_facet | Aerodynamics Luft- und Raumfahrtindustrie Aerodynamik |
| work_keys_str_mv | AT senguptatapank theoreticalandcomputationalaerodynamics |