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Low-Speed Aerodynamics

Medium: Buch
ISBN: 978-0-521-66552-0
Verlag: Cambridge University Press
Erscheinungstermin: 04.10.2010
Lieferfrist: bis zu 10 Tage

Low-speed aerodynamics is important in the design and operation of aircraft flying at low Mach number, and ground and marine vehicles. This book offers a modern treatment of the subject, both the theory of inviscid, incompressible, and irrotational aerodynamics and the computational techniques now available to solve complex problems. A unique feature of the text is that the computational approach (from a single vortex element to a three-dimensional panel formulation) is interwoven throughout. Thus, the reader can learn about classical methods of the past, while also learning how to use numerical methods to solve real-world aerodynamic problems. This second edition brings the first entirely up to date, with a new chapter on the laminar boundary layer (emphasis on the viscous-inviscid coupling), the latest versions of computational techniques, and additional coverage of interaction problems. It includes a systematic treatment of two-dimensional panel methods and a detailed presentation of computational techniques for three-dimensional and unsteady flows. With extensive illustrations and examples, this book will be useful for senior and beginning graduate-level courses, as well as a helpful reference tool for practising engineers.


Produkteigenschaften


  • Artikelnummer: 9780521665520
  • Medium: Buch
  • ISBN: 978-0-521-66552-0
  • Verlag: Cambridge University Press
  • Erscheinungstermin: 04.10.2010
  • Sprache(n): Englisch
  • Auflage: 2. Auflage 2010
  • Serie: Cambridge Aerospace Series
  • Produktform: Kartoniert, Paperback
  • Gewicht: 1167 g
  • Seiten: 630
  • Format (B x H x T): 178 x 254 x 34 mm
  • Ausgabetyp: Kein, Unbekannt
Autoren/Hrsg.

Autoren

1. Introduction and background; 2. Fundamentals of inviscid, incompressible flow; 3. General solution of the incompressible, potential flow equations; 4. Small disturbance flow over three-dimensional wings: formulation of the problem; 5. Small disturbance flow over two-dimensional airfoils; 6. Exact solutions with complex variables; 7. Perturbation methods; 8. Three-dimensional small disturbance solutions; 9. Numerical (panel) methods; 10. Singularity elements and influence coefficients; 11. Two-dimensional numerical solutions; 12. Three-dimensional numerical solutions; 13. Unsteady aerodynamics; 14. The laminar boundary layer; 15. Enhancement of the potential flow model; Appendices.