مرور Volume 7, Issue 1 بر اساس تاریخ انتشار
در حال نمایش موارد 1 - 7 از 7
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A comment on “Supply chain DEA: production possibility set and performance evaluation model (Islamic Azad University of Arak, 2010-01-01)In a recent paper in this journal, Yang et al. [Feng Yang, Dexiang Wu,Liang Liang, Gongbing Bi & Desheng Dash Wu (2009), supply chainDEA:production possibility set and performance evaluation model] defined
 
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The behavior of homological dimensions (Islamic Azad University of Arak, 2010-01-01)Let R be a commutative noetherian ring. We study the behavior of injectiveand at dimension of R-modules under the functors HomR(-,-) and -×R-.
 
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Numerical solution of seven-order Sawada-Kotara equations by homotopy perturbation method (Islamic Azad University of Arak, 2010-01-01)In this paper, an application of homotopy perturbation method is appliedto nding the solutions of the seven-order Sawada-Kotera (sSK) and a Lax'sseven-order KdV (LsKdV) equations. Then obtain the exact ...
 
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Random fixed point of Meir-Keeler contraction mappings and its application (Islamic Azad University of Arak, 2010-01-01)In this paper we introduce a generalization of Meir-Keeler contraction forrandom mapping T : Ω×C → C, where C be a nonempty subset of a Banachspace X and (Ω,Σ ) be a measurable space with being a sigma-algebra ...
 
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Approximating xed points of generalized non-expansive non-self mappings in CAT(0) spaces (Islamic Azad University of Arak, 2010-01-01)Suppose K is a nonempty closed convex subset of a complete CAT(0) spaceX with the nearest point projection P from X onto K. Let T : K → X be anonself mapping, satisfying condition (C) with F(T) :={ x ε K : Tx ...
 
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Artinianess of Graded Generalized Local Cohomology Modules (Islamic Azad University of Arak, 2010-01-01)Let R = L n2N0Rn be a Noetherian homogeneous graded ring with local basering (R0;m0) of dimension d . Let R+ = Ln2NRn denote the irrelevant idealof R and let M and N be two nitely generated graded ...
 
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Modeling, simulation and analysis of a multi degree of freedom aircraft wing model (Islamic Azad University of Arak, 2010-01-01)This paper presented methods to determine the aerodynamic forces that acton an aircraft wing during flight. These methods are initially proposed for asimplified two degree-of-freedoms airfoil model and then are ...
 



