Tests made in atmospheric wind tunnel of Nat. Advisory Comm. for Aeronautics to determine effects of pitching oscillations upon lift of airfoil; it has been found that lift of airfoil, while pitching, is usually less than that which would exist at same angle of attack in stationary condition, and that behavior of pitching airfoil may be qualitatively explained on basis of accepted aerodynamic theory.
Airfoil lift with changing angle of attack
Nat. Advisory Comm. Aeronautics -- Tech. Note
1927
15 pages
9 Figs.
Report
Englisch
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Airfoil Lift with Changing Angle of Attack
NTRS | 1927
|Airfoil lift with changing angle of attack
SLUB | 1927
|