Pressures measured on upper and lower surface at one chord section on both main airfoil and on flap for several different flap deflections and at several angles of attack; test installation was used in which airfoil was mounted horizontally in wind tunnel between vertical end planes so that two-dimensional flow was approximated. (10¢)
Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Nat Advisory Committee Aeronautics -- Report
1938
15 pages
Bibliography
Report
English
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Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Engineering Index Backfile | 1938
|Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Engineering Index Backfile | 1938
|Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap
Engineering Index Backfile | 1938
|Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap
Engineering Index Backfile | 1938
|