6th American Society for Composites Technical Conference
Abstract
A global/local procedure for the computation of the interlaminar stress components at the skin wrap, skin core, and wrap core interfaces for an advanced concept stiffened panel, is described. The procedure consists of a global model of two dimensional shell elements that is used to design a grid stiffened panel with blade type stiffeners, a local model of three dimensional solid elements that is used to compute interlaminar stress components, and a scheme devised to assign displacement boundary conditions for a local model that are based on displacement and rotation data of a few nodes of the global model. A global panel was designed according to strength, stiffness, and stability criteria associated with the design of traditional aircraft wing panels. Interlaminar normal and shearing stress components, computed via the local model, were found to be well below typical tensile normal and shearing strengths of a graphite epoxy material.
- Authors:
- Publication Date:
- Research Org.:
- National Aerospace Lab., Amsterdam (Netherlands)
- OSTI Identifier:
- 7139582
- Report Number(s):
- N-92-33139; NASA-CR-190822; NAS-1.26:190822; NLR-TP-91052-U; ETN-92-91996; CONF-9110447-
CNN: NAS1-17925
- Resource Type:
- Conference
- Resource Relation:
- Conference: 6. American Society for Composites technical conference, Albany, NY (United States), 6-9 Oct 1991
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 36 MATERIALS SCIENCE; 33 ADVANCED PROPULSION SYSTEMS; AIRCRAFT COMPONENTS; DESIGN; COMPOSITE MATERIALS; STRESS ANALYSIS; EPOXIDES; FINITE ELEMENT METHOD; GRAPHITE; LAYERS; PANELS; REINFORCED MATERIALS; SHEAR PROPERTIES; STABILITY; TENSILE PROPERTIES; CALCULATION METHODS; CARBON; ELEMENTAL MINERALS; ELEMENTS; MATERIALS; MECHANICAL PROPERTIES; MINERALS; NONMETALS; NUMERICAL SOLUTION; ORGANIC COMPOUNDS; ORGANIC OXYGEN COMPOUNDS; 360603* - Materials- Properties; 330601 - Vehicle Design Factors- Body & Chassis
Citation Formats
Wiggenraad, J F.M., and Bauld, Jr, N R. 6th American Society for Composites Technical Conference. United States: N. p., 1991.
Web.
Wiggenraad, J F.M., & Bauld, Jr, N R. 6th American Society for Composites Technical Conference. United States.
Wiggenraad, J F.M., and Bauld, Jr, N R. 1991.
"6th American Society for Composites Technical Conference". United States.
@article{osti_7139582,
title = {6th American Society for Composites Technical Conference},
author = {Wiggenraad, J F.M. and Bauld, Jr, N R},
abstractNote = {A global/local procedure for the computation of the interlaminar stress components at the skin wrap, skin core, and wrap core interfaces for an advanced concept stiffened panel, is described. The procedure consists of a global model of two dimensional shell elements that is used to design a grid stiffened panel with blade type stiffeners, a local model of three dimensional solid elements that is used to compute interlaminar stress components, and a scheme devised to assign displacement boundary conditions for a local model that are based on displacement and rotation data of a few nodes of the global model. A global panel was designed according to strength, stiffness, and stability criteria associated with the design of traditional aircraft wing panels. Interlaminar normal and shearing stress components, computed via the local model, were found to be well below typical tensile normal and shearing strengths of a graphite epoxy material.},
doi = {},
url = {https://www.osti.gov/biblio/7139582},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Wed May 01 00:00:00 EDT 1991},
month = {Wed May 01 00:00:00 EDT 1991}
}