Tests made on Clark Y airfoil with 0.20cw Clark Y Fowler flap and on N ACA 23012 airfoil with 0.20cw, 0.30cw, 0.40cw NACA 23012 Fowler flaps; test installation was used in which model was mounted in wind tunnel between large end planes so that two-dimensional flow was approximated.
Pressure distribution over airfoils with fowler flaps
Nat Advisory Committee Aeronautics -- Report
1938
19 pages
Bibliography
Report
Englisch
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Pressure distribution over airfoils with fowler flaps
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|Pressure distribution over airfoils with fowler flaps
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|THE PRACTICAL APPLICATION OF FOWLER FLAPS
SAE Technical Papers | 1937
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