The camber deformations of the flapping insect wing provide important infor
mation for lift force analysis. Recent measurements are nearly all based on
the hypothesis of the rigid wing, neglecting the camber deformation. In th
is article, a measurement system based on fringe pattern projection is intr
oduced. Projected comb fringes, whose intensity function is near a comb fun
ction, were used instead of conventional sine fringes because of their high
intensity and sharpness, allowing us to take the distorted fringes on the
transparent dragonfly wing easily. The camber deformation and torsion angle
of a flapping dragonfly wing can be measured without hypothesizing that th
e wing is a rigid plate. The experimental result shows that the camber defo
rmation is different during upstroke and downstroke. It is very important f
or the explanation of the lift force. (C) 2001 American Institute of Physic
s.