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The Effects of High-lift Devices on the Low-speed Stability of a Tapered 37.5 Degree Sweptback Wing of Aspect Ratio 3 in Straight and Rolling FlowContains results of tunnel tests to determine effects of various combinations of split flaps, slats, and nose slats on the stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow.
Document ID
19930085527
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Queijo, M J
Lichtenstein, Jacob H
Date Acquired
August 16, 2013
Publication Date
November 9, 1948
Report/Patent Number
NACA-RM-L8I03
Report Number: NACA-RM-L8I03
Accession Number
93R14817
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SLOTS AND SLATS - COMPLETE WINGS
FLAPS - COMPLETE WINGS
STABILITY, DIRECTIONAL - STATIC
STABILITY, LATERAL - STATIC
DAMPING DERIVATIVES - STABILITY
SWEEP - COMPLETE WINGS

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