2018
Reichert, Lisa; Krieglsteiner, Joscha; Schmidt, Carsten; Horst, Peter
Simplified Representation of Complex Structural Components for Finite-Element-Analysis Konferenzbeitrag
In: ECCM18, (Hrsg.): 2018.
BibTeX | Schlagwörter: Composite Structures, Modelling, Stiffener Profiles
@inproceedings{Reichert2018,
title = {Simplified Representation of Complex Structural Components for Finite-Element-Analysis},
author = {Lisa Reichert and Joscha Krieglsteiner and Carsten Schmidt and Peter Horst},
editor = {ECCM18},
year = {2018},
date = {2018-06-25},
keywords = {Composite Structures, Modelling, Stiffener Profiles},
pubstate = {published},
tppubtype = {inproceedings}
}
2014
Kriglsteiner, Joscha; Horst, Peter; Schmidt, Carsten
Optimization of fiber-reinforced stiffener profiles for aircraft fuselage preliminary structural design Konferenzbeitrag
In: 16th European Conference on Composite Materials, Seville, 2014.
Abstract | BibTeX | Schlagwörter: Composite Structures, Fuselage, Preliminary design, Stiffener Profiles
@inproceedings{Kriglsteiner2014,
title = {Optimization of fiber-reinforced stiffener profiles for aircraft fuselage preliminary structural design},
author = {Joscha Kriglsteiner and Peter Horst and Carsten Schmidt},
year = {2014},
date = {2014-06-22},
booktitle = {16th European Conference on Composite Materials},
address = {Seville},
abstract = {This paper presents a characterization module for stiffener profiles. It is part of a modellig and analysis tool for stiffened structures in aircraft fuselage design. The module offers options to determine mechanical characteristics of a given section such as mass, stiffness, and failure loads for strength and local stability. For the characterization, analytical approaches and the Finite Element Method (FEM) are used. Both ways are presented and the results are compared as part of the verification of the module. Furthermore, how the module can be used for a basic comparison of design concepts is described.},
keywords = {Composite Structures, Fuselage, Preliminary design, Stiffener Profiles},
pubstate = {published},
tppubtype = {inproceedings}
}
This paper presents a characterization module for stiffener profiles. It is part of a modellig and analysis tool for stiffened structures in aircraft fuselage design. The module offers options to determine mechanical characteristics of a given section such as mass, stiffness, and failure loads for strength and local stability. For the characterization, analytical approaches and the Finite Element Method (FEM) are used. Both ways are presented and the results are compared as part of the verification of the module. Furthermore, how the module can be used for a basic comparison of design concepts is described.