An investigation was made in the N.A.C.A. 7 by 10 foot wind tunnel of the distribution of air pressure over one chord section of a Clark Y-H airfoil with a split flap. The results obtained are given in the form of diagrams showing the chordwise distribution of pressure on both airfoil and flap as plots of calculated aerodynamic coefficients for both airfoil and flap.
Pressure distribution over a Clark Y-H airfoil section with a split flap
1937-12-01
Miscellaneous
No indication
English
Pressure distribution over clarke Y-H airfoil section with split flap
Engineering Index Backfile | 1937
|Pressure distribution over clarke Y-H airfoil section with split flap
Engineering Index Backfile | 1937
|Pressure distribution over airfoil with balanced split flap
Engineering Index Backfile | 1941
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