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12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering

Cranfield University

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Article title

Explicit dynamic formulation to demonstrate compliance against Quasi-static aircraft seat certification loads (CS25.561) - Part II: Influence of Body Blocks

Type

D - Journal article

DOI

10.1177/0954410013506415

Title of journal

Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering

Article number

Volume number

N/A

Issue number

First page of article

ISSN of journal

0954-4100

Year of publication

2013

URL

Number of additional authors

Additional information

This paper is an output from a project addressing static certification compliance of a next generation civil aircraft seat. Linking analysis-led-design, numerical simulation and experimental testing, technical outputs resulted in an automotive seat research project with Jaguar Landrover (Dr Tayeb Zegeur, tzeguer@jaguarlandrover.com). Also, sponsored by UK based SME Bluesky Designers Ltd (Dominic Robinson, djr@blueskydesignersltd.com), additional projects followed, as the company secured SEEDA (South East England Development Agency) product development grants in 2009 and 2010 for this collaboration.

Interdisciplinary

Cross-referral requested

Research group

F - Structures and Machine Systems

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract