The flow about a section of a finite-aspect-ratio NACA 0015 airfoil on a transonic bump
1953
30 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Flow about section of finite-aspect-ratio NACA-0018 airfoil on transonic bump
Engineering Index Backfile | 1953
|Vortex Developments Over NACA 0015 Airfoil with Trailing Edge Jet
British Library Conference Proceedings | 1994
|