Add to ORKGThe influence of flow and structural uncertainties on the reliability of a panel interacting with a supersonic flow are studied. First, the probability of failure of a panel with deterministic structural properties is computed by means of a conditional reliability analysis based on a first-passage formulation. Then an unconditional reliability analysis is performed in order to include the effects of structural uncertainties . Two sensitivity-based methods, the perturbation method and the fast integration method, are used to compute the unconditional probability of failure
Response of flexible structures — such as cable-supported bridges and aircraft wings — is associated...
An experimental-based approach to flutter speed uncertainty quantification in aeroelastic systems is...
In this work, a physics-based first-order reliability method (FORM) algorithm is proposed for the fl...
The influence of flow and structural uncertainties on the reliability of a panel interacting with a ...
Fluid–structure interactions provide design constraints in many fields, yet methods available for th...
Aeroelastic flutter is a dangerous failure mode, and aircraft structural components are designed und...
The field of fluid-structure interaction is combined with the field of stochastics to perform a stoc...
Fluid–structure interactions provide design constraints in many fields, yet methods available for th...
A stochastic finite element method is developed to study the reliability of structures such as beams...
The numerical simulation of multiphysics problems has grown steadily in recent years. This developme...
This study sets the framework for uncertainty propagation in hypersonic aeroelastic and aerothermoel...
Flutter-critical velocity is usually estimated from deterministic analyses by assuming that physical...
The vibration active control of the composite panels with the uncertain parameters in the hypersonic...
AbstractUncertainties denote the operators which describe data error, numerical error and model erro...
Uncertainties denote the operators which describe data error, numerical error and model error in the...
Response of flexible structures — such as cable-supported bridges and aircraft wings — is associated...
An experimental-based approach to flutter speed uncertainty quantification in aeroelastic systems is...
In this work, a physics-based first-order reliability method (FORM) algorithm is proposed for the fl...
The influence of flow and structural uncertainties on the reliability of a panel interacting with a ...
Fluid–structure interactions provide design constraints in many fields, yet methods available for th...
Aeroelastic flutter is a dangerous failure mode, and aircraft structural components are designed und...
The field of fluid-structure interaction is combined with the field of stochastics to perform a stoc...
Fluid–structure interactions provide design constraints in many fields, yet methods available for th...
A stochastic finite element method is developed to study the reliability of structures such as beams...
The numerical simulation of multiphysics problems has grown steadily in recent years. This developme...
This study sets the framework for uncertainty propagation in hypersonic aeroelastic and aerothermoel...
Flutter-critical velocity is usually estimated from deterministic analyses by assuming that physical...
The vibration active control of the composite panels with the uncertain parameters in the hypersonic...
AbstractUncertainties denote the operators which describe data error, numerical error and model erro...
Uncertainties denote the operators which describe data error, numerical error and model error in the...
Response of flexible structures — such as cable-supported bridges and aircraft wings — is associated...
An experimental-based approach to flutter speed uncertainty quantification in aeroelastic systems is...
In this work, a physics-based first-order reliability method (FORM) algorithm is proposed for the fl...