A Structural Design Concept for a Multi-Shell Blended Wing Body with Laminar Flow Control

A Structural Design Concept for a Multi-Shell Blended Wing Body with Laminar Flow Control

Static and fatigue analyses are presented for a new blended wing body (BWB) fuselage concept considering laminar flow control (LFC) by boundary layer suction in order to reduce the aerodynamic drag. BWB aircraft design concepts profit from a structurally beneficial distribution of lift and weight an...

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Bibliographic Details
Main Authors:	Majeed Bishara, Peter Horst, Hinesh Madhusoodanan, Martin Brod, Benedikt Daum, Raimund Rolfes
Format:	Article
Language:	English
Published:	MDPI AG 2018-02-01
Series:	Energies
Subjects:	blended wing body multi-bubble fuselage structural analysis controlled fiber placement fiber-reinforced plastics fatigue degradation damage model
Online Access:	http://www.mdpi.com/1996-1073/11/2/383

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