Add to ORKGLoads and aeroelasticity together influence the aircraft design and thus should be integrated in the early aircraft design. This paper presents the automated loads process, for determining the loads and load conditions, to be integrated in a multidisciplinary design process. The presented loads and sizing process comprises the load case definition, parametric modeling, loads analysis and structural sizing including aeroelastic constraints. The parametric approach set-up aeroelastic models that account for realistic constructions of an aircraft to be used for structural static and dynamic analysis. A case study is presented applied to a wide body aircraft configuration including aeroelastic assessment. The impact of aileron reversal constrai...
State of the art wing sizing in conceptual aircraft design is usually carried out by semiempirical m...
The set-up of a parametric structural finite element model for loads and aeroelastic analysis of an ...
In the preliminary design phase, aircraft are described with a limited level of detail, the focus be...
Critical loads play an essential role in early aircraft design studies. In order to determine a cons...
Multidisciplinary design is transforming the way aircraft design is performed. New challenges includ...
Loads analysis and structural design are core steps of the aircraft design process. To reduce wing l...
Loads analysis and structural design are core steps of the aircraft design process. To reduce wing l...
In order to consider a large number of design loads within the preliminary sizing process of aircraf...
Loads analysis and structural design are core steps of the aircraft design process. To reduce wing l...
The paper demonstrates a methodology that can be used at an early design stage of any conventional a...
The selection of design loads and requirements is defining the structural weight of airplanes and th...
This paper introduces a fully parameterized finite element based tool chain for the structural sizin...
The design and certification procedures of modern aircraft structures are usually based on static lo...
In this paper, a methodology is presented to size an aircraft wing-box accounting for steady and dyn...
Conceptual aircraft design uses in most cases either semi-empirical methods or simplified structural...
State of the art wing sizing in conceptual aircraft design is usually carried out by semiempirical m...
The set-up of a parametric structural finite element model for loads and aeroelastic analysis of an ...
In the preliminary design phase, aircraft are described with a limited level of detail, the focus be...
Critical loads play an essential role in early aircraft design studies. In order to determine a cons...
Multidisciplinary design is transforming the way aircraft design is performed. New challenges includ...
Loads analysis and structural design are core steps of the aircraft design process. To reduce wing l...
Loads analysis and structural design are core steps of the aircraft design process. To reduce wing l...
In order to consider a large number of design loads within the preliminary sizing process of aircraf...
Loads analysis and structural design are core steps of the aircraft design process. To reduce wing l...
The paper demonstrates a methodology that can be used at an early design stage of any conventional a...
The selection of design loads and requirements is defining the structural weight of airplanes and th...
This paper introduces a fully parameterized finite element based tool chain for the structural sizin...
The design and certification procedures of modern aircraft structures are usually based on static lo...
In this paper, a methodology is presented to size an aircraft wing-box accounting for steady and dyn...
Conceptual aircraft design uses in most cases either semi-empirical methods or simplified structural...
State of the art wing sizing in conceptual aircraft design is usually carried out by semiempirical m...
The set-up of a parametric structural finite element model for loads and aeroelastic analysis of an ...
In the preliminary design phase, aircraft are described with a limited level of detail, the focus be...