Publication Date:
2019-06-28
Description:
Wing-leading-edge modifications included leading-edge droop and slat configurations having full-span, partial-span, or segmented arrangements. Other devices included wing-chord extensions, fences, and leading-edge stall strips. Good correlation was apparent between the results of wind-tunnel data and the results of flight tests, on the basis of autorotational stability criterion, for a wide range of wing-leading-edge modifications.
Keywords:
AERONAUTICS (GENERAL)
Type:
NASA-TP-2011
,
L-15101
,
NAS 1.60:2011
Format:
application/pdf
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