Investigation conducted in Langley Memorial Aeronautical Laboratory 7 by 10-ft wind tunnel to determine air loads on airfoil in combination with fixed leading edge slot and slotted flap; pressures were measured over upper and lower surfaces of component parts of combination for several angles of attack and at several flap settings; data presented as pressure diagrams.
Pressure distribution over NACA 23012 airfoil with fixed slot and slotted flap
Nat Advisory Committee Aeronautics -- Report
1942
14 pages
Report
English
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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
|Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
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