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Journal ArticleDOI

Periodic Solutions of Gravity Oriented Axisymmetric Systems

V. J. Modi, +1 more
- 01 Feb 1974 - 
- Vol. 12, Iss: 2, pp 225-227
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TLDR
In this article, the Rayleigh quotient for the transverse vibration of a massless string under constant tension with five equal masses equally spaced along the string was derived from the simpler (and more traditional) point of view of the dynamicist.
Abstract
quadrature schemes may be used in effecting the numerical integrations. In this sense, specific discrete element "condensation" techniques represent only one of many possible ways for carrying out the required process of integration and summation in the Rayleigh-Ritz method. To further illustrate the alternative ways in which Rayleigh's principle may be applied and the fact that the use of a vibration mode determined from a first iteration does not necessarily lead to best results, the numerical example given by Fried 3 will be considered from the simpler (and more traditional) point of view of the dynamicist. The Rayleigh quotient may be formed from Fried' s Eq. (6) by multiplying the first row of the matrix equation by xl9 the second by x2, etc., and summing the results to give Ml Apart from physical constants which are absorbed in the definition of A, this may be viewed as Rayleigh's quotient for the transverse vibration of a massless string under constant tension with five equal masses equally spaced along the string. In this case the numerator represents the strain energy and the denominator represents the kinetic energy divided by frequency squared. In the traditional approach of the dynamicist, a reasonable (and typical) assumption for the shape of the lowest symmetric mode of this system would 5e a parabola (as in Appendix 1 of Ref. 4). Thus Xj_ = 5, x2 = 8, x3 = 9, x4 — 8, x5 = 5 Substituting these values into Eq. (1) gives A! - 70/259 - 0.2703 This compares to Fried's result for the singly iterated mode, A! - 0.2860, for the doubly iterated mode, ^ = 0.2680, and the exact value, Aj_ = 0.2679. The accuracy of the result obtained here by application of the primitive Rayleigh method is thus much better than the result obtained by Fried using a singly iterated mode and differs from the exact solution by less than i°/ For the an ti symmetrical case, applying a similar assumed parabola to each half of the system leads to A 2 = 1.000 which corresponds to the exact solution. By contrast, Fried obtained /2 = 1.200 for his singly iterated mode and A2 = 1.024 for his doubly iterated mode. Fried's results are a consequence of the fact that his assumed antisymmetric loading for the first iteration destroyed the subsymmetry of the first antisymmetric vibration mode in each half of the system. This example is not, of course, typical of all problems to which Rayleigh's principle might be applied. (For instance, in the bending vibration of cantilever beams of variable properties use of the first iteration for the mode shape in application of Rayleigh's principle to determination of the lowest natural frequency is often a most satisfactory procedure.) It does, however, emphasize that to obtain best results with minimum effort from Rayleigh's principle, it is necessary for the analyst to exercise a degree of judgment based on the geometrical, structural, and dynamic properties of the system under consideration and to choose analytical techniques accordingly.

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Citations
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Large-eddy simulation of pulsed high-speed subsonic jets in a turbulent crossflow

TL;DR: In this article, the effects of pulsing of high-speed subsonic jets (Ma∼0.47−0.77) on mixing and jet trajectory were investigated by using large-eddy simulation.
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Analysis of solar radiation pressure induced coupled liberations of a gravity stabilized axisymmetric satellite

TL;DR: In this paper, an analysis of solar radiation pressure induced coupled librations of gravity stabilized cylindrical spacecraft with a special reference to geostationary communication satellites is presented.
References
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Journal ArticleDOI

Periodic solutions associated with the gravity- gradient-oriented system. I - Analytical and numerical determination.

TL;DR: In this article, the authors studied the periodic solutions for an arbitrarily shaped, gravity-gradient stabilized satellite, free to librate in the orbital plane, using analytical and numerical techniques.
Journal ArticleDOI

Periodic solutions associated with the gravity- gradient-oriented system. II - Stability analysis.

TL;DR: In this paper, the stability of the periodic solutions associated with planar librations of a gravity-oriented satellite using linear perturbation analysis was studied using a stability chart in parameter space, for periodic solutions of orbital frequency.
Journal ArticleDOI

Coupled Librational Motion of an Axi-Symmetric Satellite in a Circular Orbit

TL;DR: A review of the literature suggests that the planar motion of a rigid satellite in a gravity gradient field has been the subject of considerable investigation during the past ten years as discussed by the authors, however, the dynamic study of a satellite executing librational motion out of the orbital plane has received comparatively little attention.
Journal ArticleDOI

Librations of Gravity-Oriented Satellites in Elliptic Orbits through Atmosphere

TL;DR: In this article, the coupled librational dynamics of gravity-orien ted, axisymmetric satellites in elliptic orbits are investigated and an approximate closed form solution is obtained using variation of parameter approach to study the effect of eccentricity and inertia on the response.
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