CFRP — Wing for the Alpha Jet
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 January 1987
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