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Advanced Nacelle Structures
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English
Abstract
Aircraft nacelles were originally fabricated completely out of sheet metal. Advances at Rohr have enabled the implementation of new materials in an overall effort to reduce weight and improve aircraft performance. This paper deals with new metals and their fabrication techniques as well as Polymer Matrix Composites (PMC's) and their processing techniques.
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Authors
Citation
Norris, B. and Sullivan, L., "Advanced Nacelle Structures," SAE Technical Paper 901984, 1990, https://doi.org/10.4271/901984.Also In
References
- Sullivan L. Ghaffarian R. “Microcracking Behavior of Thermally Cycled High Temperature Laminates” Conf. Proc. from 33rd International SAMPE Symposium 33 Materials-Pathways To The Future 7-10 March 1988 1604 1616
- Norris B. “Liquid Interface Diffusion (LID) Bonding of Titanium Structures” Conf. Proc. from Designing with Titanium Bristol University U.K. 7-9 July 1986
- Norris B. Gojny F. “Brazing of Titanium and Inconel Honeycomb Sandwich Components” First Int. SAMPE Conf. on Metals and Materials Cherry Hill, New Jersey August 1987
- Wittenauer J. Norris B. “High Temperature Structural Honeycomb Materials for Advanced Aerospace Designs” J.O.M. March 1990 36 41