This chapter contains sections titled:
Development of the CUSSSP Program
Exercises
Further Reading
References
Conclusion to Part I: The Origin of Lift
Panel Methods for Plane Flow
2012-07-06
14 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
complex velocity and conformal mapping, in Octave, using CUSSSP , The Kutta–Joukowsky condition , lift–incidence curve for NACA 2412, as computed by CUSSSP , panel methods for plane flow , wing sections modelled using panel methods, distributing the singularities , complete two‐dimensional wing section shapes, with thickness added , Kutta–Joukowsky condition, in determining vortex strength of panels , conformal mapping for arbitrary segments , NACA 4‐digit sections, in resolving trailing edge
Panel methods for airfoils in turbulent flow
Tema Archiv | 2010
|Panel methods for airfoils in turbulent flow
Online Contents | 2010
|Wiley | 2012
|