Wind-tunnel investigation of 20-percent-chord plain and frise ailerons on an NACA 23012 airfoil
1941
14 S., 17 Abb
Report
English
Wind-tunnel investigation of 20-percent-chord plain and frise ailerons on NACA 23012 airfoil
Engineering Index Backfile | 1941
|Wind-tunnel investigation of NACA 23012 airfoil with 30-percent-chord venetian-blind flaps
Engineering Index Backfile | 1942
|