University of North Texas Digital Library (University of North Texas) · 1940 · 154 citations · 0 references
Open access
EngineeringAerospace EngineeringMechanical EngineeringAerodynamicsStructural EngineeringVibrationExperimental AerodynamicsVibration AnalysisWind-induced VibrationWing AerodynamicsWing StructuresWing TheoryCantilever MechanicsExperimental Results InterpretationFlutterFlutter AnalysisTaper EffectsVibration ModesWing FlutterWing Flutter Analysis
From Summary: "The results of the basic flutter theory originally devised in 1934 and published as NACA Technical Report no. 496 are presented in a simpler and more complete form convenient for further studies. The paper attempts to facilitate the judgement of flutter problems by a systematic survey of the theoretical effects of the various parameters. A large number of experiments were conducted on cantilever wings, with and without ailerons, in the NACA high-speed wind tunnel for the purpose of verifying the theory and to study its adaptability to three-dimensional problems."