Wind-tunnel investigation of control-surface characteristics ; 16: Pressure distribution over an NACA 0009 airfoil with 0.30-airfoil-chord beveled-trailing-edge flaps
Wartime report ; L-205
1944
22 S., [48] Bl
Originally issued April 1944 as Advance restricted report L4D03
Book
English
Engineering Index Backfile | 1948
|Engineering Index Backfile | 1948
|Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
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