The Stability Of Momentless Cylindrical Membrane Shell In Supersonic Gas Flow
Journal Title: Հայաստանի գիտությունների ազգային ակադեմիայի տեղեկագիր․ Մեխանիկա - Year 2006, Vol 59, Issue 2
Abstract
The stability of momentless cylindrical membrane shell in the two-dimensional flow of gas is investigated here. The areas of instability are compared according to “piston” theory and the one of precise approximation, when the aerodynamical pressure dependence from the motion of membrane has non-local character of differential type. Unlike the “piston” theory, the calculations according to the theory of precise approximation show the instability of membrane under the small supersonic numbers of Mach. At the same time the upper verge (border) of stability area is considerably reduced as well.
Authors and Affiliations
L. A. Vanyan
About interaction of finite and semi-finite cracks in elastic half-plane.
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Optimum Stochastle Control of Doublelink Electromechanical manipulator.
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The plane problem in the creep theory for a finite thickness layer.
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On statistical models of fatigue life at random loading with single overloads.
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Extended orthogonality relations to solve boundary problems in the theory of elasticity.
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