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
English
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Pressure distribution over airfoils with Fowler flaps
TIBKAT | 1938
|Pressure distribution over airfoils with fowler flaps
Engineering Index Backfile | 1938
|Pressure distribution over airfoils with fowler flaps
Engineering Index Backfile | 1938
|THE PRACTICAL APPLICATION OF FOWLER FLAPS
SAE Technical Papers | 1937
|Lift Augmentation on Hollow Airfoils with Flaps
British Library Conference Proceedings | 2001
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