Pressure distribution tests of Clark Y airfoil with flap and inset tab measured on both upper and lower surfaces at one chord section; calculations of normal force and pitching moment coefficients of airfoil section and normal force and hinge moment coefficients of flap section with tab, also normal force and hinge moment coefficients of tab section alone; comparisons of theoretical and experimental values. (10c)
Pressure distribution over airfoil section with flap and tab
Nat Advisory Committee Aeronautics -- Report
1936
11 pages
Bibliography
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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
|