The Integration of Composite Structures into Aircraft Design-Reference-Cited by-同舟云学术

The Integration of Composite Structures into Aircraft Design

Published:1972-04 Issue:2 Volume:6 Page:174-190
ISSN:0021-9983
Container-title:Journal of Composite Materials
language:en
Short-container-title:Journal of Composite Materials

Author:

Waddoups M.E.¹,Jackson S.K.¹,Rogers C.W.¹

Affiliation:

1. General Dynamics Convair Aerospace Division Fort Worth, Texas 76101

Abstract

Advanced composite materials are significantly different from conven tional aircraft materials. These differences between the two are such that all facets of airplane design are significantly affected when use of advanced composite materials is considered. Examples of the impact of composite application to a lightweight fighter design, with regard to configuration and structural integrity, are given in this paper.

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Link

http://journals.sagepub.com/doi/pdf/10.1177/002199837200600201

Reference9 articles.

1. Macroscopic Fracture Mechanics of Advanced Composite Materials

2. A General Theory of Strength for Anisotropic Materials

3. The Brittle Strength of Orthotropic Materials

4. M.E. Waddoups, "Characterization and Design of Composite Materials," Composite Materials Workshop, Ed. S. W. Tsai , et al. Technomic (1968), p. 258.

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