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An analysis of the factors affecting the loss in lift and shift in aerodynamic center produced by the distortion of a swept wing under aerodynamic load
Document ID
19930083589
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mathews, Charles W
Kurbjun, Max C
Date Acquired
August 16, 2013
Publication Date
March 1, 1953
Report/Patent Number
NACA-TN-2901
Report Number: NACA-TN-2901
Accession Number
93R12879
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, COMPLETE - ASPECT RATIO
WING SECTIONS - THICKNESS
WINGS, COMPLETE - SWEEP
AIRPLANES - COMPONENTS IN COMBINATION
WING SECTIONS
WINGS, COMPLETE - TAPER AND TWIST
AEROELASTICITY
STABILITY, LONGITUDINAL - STATIC

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