The shapes of bodies with maximum lift-to-drag ratio in supersonic flow

Assuming that the pressure coefficient on the body surface is defined by the angle between the local normal to it and the velocity vector of the undisturbed flow, the problem of the shape of a body which possesses the maximum lift-to-drag ratio is solved. When the bottom section area and the constan...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of applied mathematics and mechanics 2009, Vol.73 (5), p.514-523
Hauptverfasser:	Lapygin, V.I., Yakunina, G.Ye
Format:	Artikel
Sprache:	eng
Schlagworte:	Angle of attack Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Mathematical analysis Optimization Physics Planes Supersonic and hypersonic flows Supersonic flow Two dimensional Vectors (mathematics) Wedges
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!