No abstract

Nomenclature-curve slope, 1/deg C M = pitching-moment coefficient about quarter-chord point of the root chord, = M/(0.5ρV 2 Sc) c 0 = root chord measured along the longitudinal axis of the winḡ c = mean aerodynamic chord measured along the longitudinal axis D = drag force d = position of the maximum reflex h i = height of the maximum inverse camber h z = camber height at z cross section in spanwise direction h 0 = camber height at the root of the wing L = lift force M = pitching moment about quarter-chord point of the root chord m = mass Re = mean-aerodynamic-chord Reynolds number S = wing planform area T P = thrust force