Wind-tunnel investigation of 20-percent-chord plain and Frise ailerons on an NACA 23012 airfoil
1941-12-01
Sonstige
Keine Angabe
Englisch
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
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