Publication Date:
2019-06-28
Description:
The wind tunnel testing of an advanced technology high lift system for a wide body and a narrow body transport incorporating high aspect ratio supercritical wings is described. This testing has added to the very limited low speed high Reynolds number data base for this class or aircraft. The experimental results include the effects on low speed aerodynamic characteristics of various leading and trailing edge devices, nacelles and pylons, ailerons, and spoilers, and the effects of Mach and Reynolds numbers.
Keywords:
AERODYNAMICS
Type:
NASA-CR-3523
,
NAS 1.26:3523
,
ACEE-17-FR-1608
Format:
application/pdf
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