Tests in the compressed air tunnel on the aerofoils NACA 0015 and NACA 0030 with and without split flap and other aerofoils of various thickness with a split flap
1952
32 S.
graph. Darst.
Report
English
Pressure distribution over NACA 23021 airfoil with slotted and split flap
Engineering Index Backfile | 1941
|Wind-tunnel investigation of NACA 23012 airfoil with two sizes of balanced split flap
Engineering Index Backfile | 1940
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