Unsteady Characteristics of Thrust and Lift Acting on a Heaving Airfoil
نویسندگان
چکیده
منابع مشابه
Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula
A = heaving amplitude, m Cl = lift coefficient c = wing chord, m Dbl = boundary-layer domain Dout = outer flow domain F = aerodynamic force, N f = flapping frequency, s−1 k = πfc∕U, reduced frequency k = unit vector normal to the freestream velocity L, L 0 = lift or sectional lift, N or N · m−1 La, L 0 a = lift or sectional lift associated with the fluid acceleration, N or N · m−1 Lvor, L 0 vor...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
سال: 2005
ISSN: 0387-5016,1884-8346
DOI: 10.1299/kikaib.71.104