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Rizzi / Oppelstrup

Aircraft Aerodynamic Design with Computational Software

Medium: Buch
ISBN: 978-1-107-01948-5
Verlag: Cambridge University Press
Erscheinungstermin: 20.05.2021
Lieferfrist: bis zu 10 Tage

This modern text presents aerodynamic design of aircraft with realistic applications, using CFD software and guidance on its use. Tutorials, exercises, and mini-projects provided involve design of real aircraft, ranging from straight to swept to slender wings, from low speed to supersonic. Supported by online resources and supplements, this toolkit covers topics such as shape optimization to minimize drag and collaborative designing. Prepares seniors and first-year graduate students for design and analysis tasks in aerospace companies. In addition, it is a valuable resource for practicing engineers, aircraft designers, and entrepreneurial consultants.


Produkteigenschaften


  • Artikelnummer: 9781107019485
  • Medium: Buch
  • ISBN: 978-1-107-01948-5
  • Verlag: Cambridge University Press
  • Erscheinungstermin: 20.05.2021
  • Sprache(n): Englisch
  • Auflage: Erscheinungsjahr 2021
  • Produktform: Gebunden
  • Gewicht: 977 g
  • Seiten: 465
  • Format (B x H x T): 175 x 250 x 29 mm
  • Ausgabetyp: Kein, Unbekannt
Autoren/Hrsg.

Autoren

Arthur Rizzi is Professor of Aeronautics at the KTH Royal Institute of Technology. He is the recipient of the Royal Aeronautical Society's Busk Prize, and the Swedish Aeronautics and Astronautics Society's Thulin Medal.

Jesper Oppelstrup is Professor of Numerical Analysis at the KTH Royal Institute of Technology with practical experience in industry of applying computational mathematics.

1. Introduction to Aircraft Aerodynamic Design; 2. Airflow Physics and Mathematical Models; 3. Concepts and Computational Models in Wing Design; 4. Finite Volume Schemes for the Euler Equations; 5. Airframe CAD and Automated Grid Generation; 6. CFD for Steady and Unsteady Flows; 7. Fast Computation of Airfoil Flow; 8. Airfoil Design Considerations; 9. Wing Design Considerations; 10. Configuration Development and Flying Qualities; 11. Airload-Structure Interaction and Aeroelastic Effects.