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Effect of Finite Span on the Airload Distributions for Oscillating Wings I : Aerodynamic Theory of Oscillating Wings of Finite Span
Document ID
19930082160
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Reissner, Eric (Massachusetts Institute of Technology)
Date Acquired
August 16, 2013
Publication Date
March 1, 1947
Report/Patent Number
NACA-TN-1194
Report Number: NACA-TN-1194
Accession Number
93R11450
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER - WINGS
THEORIES - AIRFOILS LIFTING-LINE
LIFT DISTRIBUTION, WING-SPAN
WINGS - BENDING & TORSION
PRESSURE DISTRIBUTION - WINGS
LOAD DISTRIBUTION, WING-SPAN
WINGS - OSCILLATIONS
THEORIES - AIRFOILS LIFTING-SURFACE
EQUATIONS - FLUTTER
THEORIES - WINGS FLUTTER

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