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Calculated effects of geometric dihedral on the low-speed rolling derivatives of swept wings
Document ID
19930082427
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Queijo, M J
Jaquet, Byron M
Date Acquired
August 16, 2013
Publication Date
October 1, 1948
Report/Patent Number
NACA-TN-1732
Report Number: NACA-TN-1732
Accession Number
93R11717
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - NACA - STABILITY WORK CARRIED ON AT LAL
DAMPING IN ROLL
AIRFOILS - NACA 0012
ROLLING & YAWING MOMENTS - WINGS, SWEPTBACK
WINGS, SWEPTBACK - STABILITY, LATERAL
WINGS - DIHEDRAL
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