A comparison of hinge moments of flaps on N.A.C.A. 4412 as determined by theory and experiment
1941
10 S.
4°
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Calculated and measured pressure distributions over midspan section of N.A.C.A. 4412 airfoil
Engineering Index Backfile | 1936
|Engineering Index Backfile | 1936
|Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flaps
Engineering Index Backfile | 1938
|