The theoretical stability derivatives for a symmetrically tapered wing of aspect-ratio 3 at supersonic speeds
1966
4 S., 3 Bl. graph. Darst.
4"
[Umschlagt.]
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds
Engineering Index Backfile | 1947
|Computational Study of a Conical Unit Aspect Ratio Wing at Supersonic Speeds
Online Contents | 1995
|