Drag Tests of an NACA 65(215)-114, a = 1.0 Practical-construction Airfoil Section Equipped with a 0.295-airfoil-chord Slotted Flap
1947-04-01
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1947
|Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
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