Andere Kunden interessierten sich auch für
![Finite Element Model Optimization of the FalconSAT-5 Structural Engineering Model]( "Finite Element Model Optimization of the FalconSAT-5 Structural Engineering Model")
Finite Element Model Optimization of the FalconSAT-5 Structural Engineering Model63,99 €![Finite Element A Posteriori Error Estimation for Heat Conduction]( "Finite Element A Posteriori Error Estimation for Heat Conduction")
Finite Element A Posteriori Error Estimation for Heat Conduction64,99 €![Finite Element Analysis of Active and Sensory Thermopiezoelectric Composite Materials]( "Finite Element Analysis of Active and Sensory Thermopiezoelectric Composite Materials")
Finite Element Analysis of Active and Sensory Thermopiezoelectric Composite Materials64,99 €![Process for Refining and Validating a Finite Element Model of an Experimental High-Altitude, Long-Endurance (Hale) Aircraft]( "Process for Refining and Validating a Finite Element Model of an Experimental High-Altitude, Long-Endurance (Hale) Aircraft")
Process for Refining and Validating a Finite Element Model of an Experimental High-Altitude, Long-Endurance (Hale) Aircraft64,99 €![Finite Element Solution: Nonlinear Flapping Beams for Use with Micro Air Vehicle Design]( "Finite Element Solution: Nonlinear Flapping Beams for Use with Micro Air Vehicle Design")
Finite Element Solution: Nonlinear Flapping Beams for Use with Micro Air Vehicle Design63,99 €![Least-Squares Finite Element Formulation for Fluid-Structure Interaction]( "Least-Squares Finite Element Formulation for Fluid-Structure Interaction")
Least-Squares Finite Element Formulation for Fluid-Structure Interaction63,99 €![The Development of a Finite Element Program to Model High Cycle Fatigue in Isotropic Plates]( "The Development of a Finite Element Program to Model High Cycle Fatigue in Isotropic Plates")
The Development of a Finite Element Program to Model High Cycle Fatigue in Isotropic Plates63,99 €
The displacement formulation of the finite element method is the most general and most widely used technique for structural analysis of airplane configurations. Modem structural synthesis techniques based on the finite element method have reached a certain maturity in recent years, and large airplane structures can now be optimized with respect to sizing type design variables for many load cases subject to a rich variety of constraints including stress, buckling, frequency, stiffness and aeroelastic constraints (Refs. 1-3). These structural synthesis capabilities use gradient based nonlinear programming techniques to search for improved designs. For these techniques to be practical a major improvement was required in computational cost of finite element analyses (needed repeatedly in the optimization process). Thus, associated with the progress in structural optimization, a new perspective of structural analysis has emerged, namely, structural analysis specialized for design optimization application, or.what is known as "design oriented structural analysis" (Ref. 4). This discipline includes approximation concepts and methods for obtaining behavior sensitivity information (Ref. 1), all needed to make the optimization of large structural systems (modeled by thousands of degrees of freedom and thousands of design variables) practical and cost effective.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.