AV-SB/GR Mk 5 Airframe Composite Applications

Autor:	B L Riley
Rok vydání:	1986
Předmět:	Engineering Fuselage business.industry Composite wing Airframe Composite number General Engineering General Medicine Structural engineering business
Zdroj:	Proceedings of the Institution of Mechanical Engineers, Part D: Transport Engineering. 200:167-183
ISSN:	0265-1904
DOI:	10.1243/pime_proc_1986_200_178_02
Popis:	This paper describes the composite applications on the AV-8B/GR Mk 5 Harrier II airfame. Twenty-five per cent of the airframe weight is composite materials resulting in a weight saving of 525 lb per aircraft. Topics covered in this paper include the composite wing, forward fuselage and horizontal tail designs, the development test programmes, design philosophy, interpretation and evaluation of test results, impact damage, ballistic damage, lightning, repairs, and manufacturing defects.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::7e0638f57492f4631fc1c7905aba4a08 https://doi.org/10.1243/pime_proc_1986_200_178_02 Zobrazit plný text záznamu