AIRCRAFT WINGS HAVING CONTINUOUSLY TAILORED STRUCTURAL STRENGTH

The structural strength of an aircraft wing is continuously tailored along its length to closely match continuously varying imposed wing loads. The wing comprises upper and lower skins each formed from panels joined together. Each of the skin panels includes a stiffening web sandwiched between and j...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PRICHARD ALAN KEITH, STUHR VICTOR, OLIVADOTI JOSEPH R
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!