Refinement and analysis of concept

• High lift device
Refinement of wing
– Leading edge high lift devices
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• While leading edge high lift devices may be located across the greater part
of the wing span, it may be necessary to accept some interruption, as for
example in the region of wing-located powerplants.
• Such effects should be minimised and carefully considered as the details of
the design are established.
Aircraft Conceptual Design