Aircraft Engineering and Aerospace Technology: Volume 71 Issue 1

Strapline:

An International Journal
Subjects:

Table of contents

Crashworthiness of helicopter subfloor structural components

Chiara Bisagni

The present investigation is oriented towards the design of an energy absorbing aluminium subfloor for a new Agusta helicopter. To identify the detailed design and the structural…

1244

Numerical simulation of crashworthiness with an implicit finite element code

D. Graillet, J.‐P. Ponthot

Implicit and explicit time integration schemes in conjunction with the finite element method are presented for the transient response of highly non‐linear problems such as impact…

Vibration reduction and monitoring

Terry Ford

Typical passive and active vibration reduction systems are dealt with, particular emphasis being on the Westland active control of structural response system fitted to all…

892

Composite design software reduces engineering time on Eurofighter parts

Tony Williams, Brian Birchall, Julian Rishton

Composite design software is helping engineers from British Aerospace to reduce significantly engineering time on composite parts for the Eurofighter 2000 aircraft. FiberSIM’…

646

Lockheed Martin: an industry leader with a compelling vision achieves software superiority and competitive edge

Tani Haque

Details developments at Lockheed Martin using process‐based software configuration management (SCM).

502

Touchscreen technology ‐ breakthrough for hardness testing

Trevor Sidaway

Briefly discusses the development of touchscreen testing for use in hardness testing for analysis and control.

404

Boeing enters new era in military aircraft production

Western Data Systems

Discusses the implementation of a new integrated manufacturing control system from Western Data Systems at Boeing.

3535

Tiltrotor progress

Terry Ford

Outlines the development work on the tiltrotor undertaken during past decades and the more recent progress on the V‐22 Osprey now in production for the US Armed Forces. Also…

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Cover of Aircraft Engineering and Aerospace Technology

ISSN:

0002-2667

Online date, start – end:

1929

Copyright Holder:

Emerald Publishing Limited

Open Access:

hybrid

Editor:

  • Prof Phil Webb