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The Effect of Negative Dihedral, Tip Droop, and Wing-tip Shape on the Low-speed Aerodynamic Characteristics of a Complete Model Having a 45 Degrees Sweptback WingAn investigation has been conducted in the Langley 300 MPH 7- by 10-foot tunnel to determine the effect of negative dihedral, tip droop, and wing-tip shape on the low-speed aerodynamic characteristics of a complete model having a 45 degrees sweptback wing. Longitudinal and lateral stability characteristics were obtained for the model with and without tail surfaces.
Document ID
19930085498
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spearman, M Leroy
Becht, Robert E
Date Acquired
August 16, 2013
Publication Date
December 6, 1948
Report/Patent Number
NACA-RM-L8J07
Report Number: NACA-RM-L8J07
Accession Number
93R14788
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY, LONGITUDINAL - STATIC
SWEEP - COMPLETE WINGS
STABILITY, LATERAL - STATIC
STABILITY, DIRECTIONAL - STATIC

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