Nonweiler, T.
Description:
We shall attempt here to summarise the existing
data on the values of the low-speed CLmax of wings,
in the absence of a fuselage, and without including
information on stalling incidence or pitching moment.
The summary is limited to the consideration of
unswept wings, and those of delta planforms, which
have symmetrical sections: there is some discussion
of the maximum lift increments due to the use of
flaps of various kinds.