A test installation was used in which an airfoil of 7-foot span was mounted vertically between the upper and the lower sides of the closed test section so that two-dimensional flow was approximated.
Wind-Tunnel Investigation of an N.A.C.A. 23012 Airfoil with a Slotted Flap and Three Types of Auxiliary Flap
01.01.1939
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1939
|Tests of N.A.C.A 23012 airfoil with slotted deflector flap
Engineering Index Backfile | 1939
|Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Engineering Index Backfile | 1938
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