770 research outputs found

    The Administration of Public Assistance

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    This Essay discusses the problems of implementation and administration of proposed welfare reforms. It gives a brief historical background on such reforms, describes the nature of their administration, discusses current and proposed reforms and the public perceptions of them, and compares welfare to other government expenditures. It concludes by recommending that social services be integrated at the local rather than federal level

    Two-dimensional global manifolds of vector fields

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    We describe an efficient algorithm for computing two-dimensional stable and unstable manifolds of three-dimensional vector fields. Larger and larger pieces of a manifold are grown until a sufficiently long piece is obtained. This allows one to study manifolds geometrically and obtain important features of dynamical behavior. For illustration, we compute the stable manifold of the origin spiralling into the Lorenz attractor, and an unstable manifold in zeta(3)-model converging to an attracting limit cycle

    Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System

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    Effects of Freeplay on Dynamic Stability of an Aircraft Main Landing Gear

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    A bifurcation study to guide the design of a landing gear with a combined uplock/downlock mechanism

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    This paper discusses the insights that a bifurcation analysis can provide when designing mechanisms. A model, in the form of a set of coupled steady-state equations, can be derived to describe the mechanism. Solutions to this model can be traced through the mechanism's state versus parameter space via numerical continuation, under the simultaneous variation of one or more parameters. With this approach, crucial features in the response surface, such as bifurcation points, can be identified. By numerically continuing these points in the appropriate parameter space, the resulting bifurcation diagram can be used to guide parameter selection and optimization. In this paper, we demonstrate the potential of this technique by considering an aircraft nose landing gear, with a novel locking strategy that uses a combined uplock/downlock mechanism. The landing gear is locked when in the retracted or deployed states. Transitions between these locked states and the unlocked state (where the landing gear is a mechanism) are shown to depend upon the positions of two fold point bifurcations. By performing a two-parameter continuation, the critical points are traced to identify operational boundaries. Following the variation of the fold points through parameter space, a minimum spring stiffness is identified that enables the landing gear to be locked in the retracted state. The bifurcation analysis also shows that the unlocking of a retracted landing gear should use an unlock force measure, rather than a position indicator, to de-couple the effects of the retraction and locking actuators. Overall, the study demonstrates that bifurcation analysis can enhance the understanding of the influence of design choices over a wide operating range where nonlinearity is significant

    Upset Dynamics of an Airliner Model: A Nonlinear Bifurcation Analysis

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    Investigation into the interaction of nose landing gear and two DOF fuselage dynamics

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