ESDU TM 216
ESDU TECHNICAL MEMORANDUM
Derivations of equations for profile drag increment conversion factors for part-span flaps
Abstract:
Derivations for the profile drag increment conversion factor equations for part-span flaps, provided in ESDU Aero F.02.01.07, are given. The derivations of the equations for straight-tapered wings and for elliptic wings are presented.Indexed under:
Details:
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