Journal of Applied Mechanics, Volume 15American Society of Mechanical Engineers, 1948 - Mechanical engineering |
Contents
The Bending of Symmetrically Loaded Circular Plates of Variable Thickness | 1 |
Critical Shear Stress of Plates Above the Proportional Limit George Gerard | 7 |
The Flutter of a Uniform Wing With Tip Weights Martin Goland and Y L Luke | 13 |
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Common terms and phrases
aluminum analysis Applied Mechanics Division ASME authors axial axis beam bearing bending blade calculated cantilever cent coefficient components compression computed constant cutting cutting fluid cylinder damping dashpot deflection deformation determined dimensionless discussion displacement effect elastic energy Equa Equation experimental flow fluid flutter force fracture frequency friction function gage given Grignard reagent hole Hooke's law hydrosphere impact JOURNAL OF APPLIED linear load longitudinal mass material maximum measured MECHANICAL ENGINEERS metal method mode shapes modes modulus motion obtained parameters plastic plate Poisson's ratio present pressure problem radial radius Rayleigh reinforcement shear modulus shear strain shear stress shown in Fig solution specimen speed steel strain energy stress ratio stress-strain curve surface symmetrical Table tangential temperature tension tests theoretical theory thickness tion torsion tube turbulence values variable velocity vibration wing zero