Calculation of the aerodynamic characteristics of tapered wings with partial-span flaps (1939)
NASA Technical Reports Server (NTRS) · leaf 5
efore the flap is deflected. distribution as long as they are symmetrical about the If this initial angle is measured from the chord of the wing center. For example, if flaps of uniform flap- root section, as is usually the case, the angle of zero chord ratio extend from 0.36 to 0.76, the proper… … bf/b Flap span/wing span, must be used because the slope of the sections with flaps FjCiUUE 2.—Factor of angle of zero lift, /. may be considerably different from the slope of the
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
