Recent content by cptcolo
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Spanwise Lift force distribution?
Ken, Spanwise lift coefficient is what you multiply the local CL by. An elliptical wing is 1 across the entire semi-span (root end to tip). Most wings have taper and are defined by a taper ratio (tip end cord length/root end cord length). For most straight wings the spanwise lift coefficient...- cptcolo
- Post #6
- Forum: Aerospace Engineering