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CFRP — Wing for the Alpha Jet

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 January 1987

91

Abstract

The end of the development chain of plane load bearing structures in CFRP‐technology after Air brake (series operation), vertical tail rudder (longtime evaluation during operation) and horizontal stabiliser (test flight programme successfully accomplished) is the pressurised wing, designed and manufactured for comprehensive structural tests.

Citation

Rose, D. (1987), "CFRP — Wing for the Alpha Jet", Aircraft Engineering and Aerospace Technology, Vol. 59 No. 1, pp. 10-13. https://doi.org/10.1108/eb036386

Publisher

:

MCB UP Ltd

Copyright © 1987, MCB UP Limited

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