The formulation basis for establishing the static or dynamic equilibrium configurations of finite element models of structures which may behave in the nonlinear range are provided. With both geometric and time independent material nonlinearities included, the development is restricted to simple one and two dimensional finite elements which are regarded as being the basic elements for modeling full aircraft-like structures under crash conditions. Representations of a rigid link and an impenetrable contact plane are added to the deformation model so that any number of nodes of the finite element model may be connected by a rigid link or may contact the plane. Equilibrium configurations are derived as the stationary conditions of a potential f...
The monograph was prepared to give the practicing engineer a clear understanding of dynamics with sp...
Program predicts expected deformations and stresses in nonlinear simple geometric structures subject...
The DYLOFLEX computer program system expands the aeroelastic cycle from that in the FLEXSTAB compute...
The formulation basis for nonlinear transient analysis of finite element models of structures using ...
An evaluation of the ACTION computer code on an aircraft like structure is presented. This computer ...
Topics addressed include: transient dynamics; transient finite element method; transient analysis in...
With increasing requirements for lower emissions and costs, next-generation transport aircraft are p...
The structural analysis methods research has several goals. One goal is to develop analysis methods ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
A computational procedure is presented for the nonlinear dynamic analysis of unsymmetric structures ...
The primary aim of this study is to understand and implement in a computer program the basic theory ...
Recently, the interest in monitoring the structural health of dynamic systems has been increasing. E...
AGGIE 1 is a computer program for predicting the linear and nonlinear, static and dynamic structural...
A general discrete methodology for modeling the dynamics of a mass that moves on the surface of a fl...
The technical progress of researches on alternatives for jet engine control is reported. Extensive n...
The monograph was prepared to give the practicing engineer a clear understanding of dynamics with sp...
Program predicts expected deformations and stresses in nonlinear simple geometric structures subject...
The DYLOFLEX computer program system expands the aeroelastic cycle from that in the FLEXSTAB compute...
The formulation basis for nonlinear transient analysis of finite element models of structures using ...
An evaluation of the ACTION computer code on an aircraft like structure is presented. This computer ...
Topics addressed include: transient dynamics; transient finite element method; transient analysis in...
With increasing requirements for lower emissions and costs, next-generation transport aircraft are p...
The structural analysis methods research has several goals. One goal is to develop analysis methods ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
A computational procedure is presented for the nonlinear dynamic analysis of unsymmetric structures ...
The primary aim of this study is to understand and implement in a computer program the basic theory ...
Recently, the interest in monitoring the structural health of dynamic systems has been increasing. E...
AGGIE 1 is a computer program for predicting the linear and nonlinear, static and dynamic structural...
A general discrete methodology for modeling the dynamics of a mass that moves on the surface of a fl...
The technical progress of researches on alternatives for jet engine control is reported. Extensive n...
The monograph was prepared to give the practicing engineer a clear understanding of dynamics with sp...
Program predicts expected deformations and stresses in nonlinear simple geometric structures subject...
The DYLOFLEX computer program system expands the aeroelastic cycle from that in the FLEXSTAB compute...