524
P. Liu
In the design of the actual aircraft lifting device, it is also necessary to
carry out the design of the retracting mechanism and structure. After careful
aerodynamic design, the leading edge slat and trailing edge flap require a
Fig. 7.103 Flow field around three-segment wing with leading slat and trailing
Fowler flap
Fig. 7.104 Detached wake from discontinuity of the trailing edge of the lifting
device