Energy Dissipation in Spacecraft Structures Incorporating Bolted Joints Operating in Macroslip-Reference-Cited by-同舟云学术

Energy Dissipation in Spacecraft Structures Incorporating Bolted Joints Operating in Macroslip

Published:2008-01 Issue:1 Volume:21 Page:19-26
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wang R.¹²³¹,Crocombe A. D.¹²³¹,Richardson G.¹²³¹,Underwood C. I.¹²³¹

Affiliation:

1. Univ. of Surrey, Guildford, Surrey GU2 7XH, U.K.

2. Professor, School of Engineering, Univ. of Surrey, Guildford, Surrey GU2 7XH, U.K. (corresponding author). E-mail: a.crocombe@surrey.ac.uk

3. Surrey Space Technology Ltd., Guildford, Surrey GU2 7XH, U.K.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282008%2921%3A1%2819%29

Reference14 articles.

1. Estimating the energy dissipated in a bolted spacecraft at resonance

2. Esmailzadeh E. and Chorashi M. (1996). “Optimal design of preloaded joints under dynamic loadings.” Proc. Int. Conf. on Pressure Vessel Technology Vol. 2 ICPVT Montreal 7–13.

3. Analysis of Preloaded Bolted Joints Under Exponentially Decaying Pressure

4. Influence of equivalent bolt length in finite element modeling of T-stub steel connections

5. Nonlinear dynamics of structures assembled by bolted joints

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