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Ground Effects on the Longitudinal Characteristics of Two Models with Wings Having Low Aspect Ratio and Pointed TipsWind-tunnel tests were conducted to determine the ground effects on a tailless model with a wing of aspect ratio 2 and infinite taper, and on a tailed model with a triangular wing of aspect ratio 3, with flaps. Control-surface hinge moments were measured on the tailless model. The results are compared with the predictions of the theory of Tani, et al.
Document ID
19930084743
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Buell, Donald A
Tinling, Bruce E
Date Acquired
August 16, 2013
Publication Date
July 1, 1957
Report/Patent Number
NACA-TN-4044
Report Number: NACA-TN-4044
Accession Number
93R14033
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROLS, FLAP-TYPE - COMPLETE WINGS
WING-FUSELAGE COMBINATIONS - AIRPLANES
TAIL-WING-FUSELAGE COMBINATIONS - AIRPLANES
CONTROL, HINGE MOMENTS
CONTROL, LONGITUDINAL
FLAPS, TRAILING-EDGE - COMPLETE WINGS
STABILITY, LONGITUDINAL - STATIC
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