Section characteristics of the NACA 0006 airfoil with leading-edge and trailing-edge flaps
1956
17 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Section characteristics of NACA 0006 airfoil with area suction near leading edge
Engineering Index Backfile | 1954
|Unsteady Airfoil with Dynamic Leading- and Trailing-Edge Flaps
Online Contents | 2009
|