Find Research Outputs

Search in all content

Filters for Research Output

Search concepts
Selected filters

Publication Year

  • 2020
  • 2019
  • 2018
  • 2017
  • 2016
  • 2015
  • 2014
  • 2013
  • 2012
  • 2011

Author

  • Richard Butler
2012

A variational model for the wrinkling of carbon fiber composites during consolidation

Dodwell, T., Butler, R. & Hunt, G. W., 2012.

Research output: Contribution to conferencePaper

Bending strength of delaminated aerospace composites

Kinawy, M., Butler, R. & Hunt, G. W., 28 Apr 2012, In : Philosophical Transactions of the Royal Society A - Mathematical Physical and Engineering Sciences. 370, 1965, p. 1780-1797 18 p.

Research output: Contribution to journalArticle

Open Access
File
14 Citations (Scopus)
129 Downloads (Pure)

Buckling optimization of variable angle tow panels using exact strip models

Liu, W., Butler, R. & Kim, H. A., 2012.

Research output: Contribution to conferencePaper

1 Citation (Scopus)

Compressive strength following delamination induced interaction of panel and sublaminate buckling

Rhead, A. T., Butler, R. & Hunt, G. W., 1 Dec 2012, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Citations (Scopus)

Compressive strength of delaminated aerospace composites

Butler, R., Rhead, A. T., Liu, W. & Kontis, N., 28 Apr 2012, In : Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences. 370, 1965, p. 1759-1779 21 p.

Research output: Contribution to journalArticle

Open Access
File
37 Citations (Scopus)
133 Downloads (Pure)

Damage tolerance of fully orthotropic laminates in compression

Baker, N., Butler, R. & York, C. B., 8 Jun 2012, In : Composites Science and Technology. 72, 10, p. 1083-1089 7 p.

Research output: Contribution to journalArticle

Open Access
File
14 Citations (Scopus)
156 Downloads (Pure)
9 Citations (Scopus)
216 Downloads (Pure)

Growth of damage in additively manufactured metal-composite joints

Parkes, P. N., Butler, R. & Almond, D. P., 2012.

Research output: Contribution to conferencePaper

16 Citations (Scopus)

The effect of tow gaps on compression after impact strength of AFP laminates

Rhead, A. T., Dodwell, T. J. & Butler, R., 2012.

Research output: Contribution to conferencePaper

1 Citation (Scopus)

The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination

Rhead, A. T., Butler, R., Liu, W. & Baker, N., Dec 2012, In : Aeronautical Journal. 116, 1186, p. 1315-1330 16 p.

Research output: Contribution to journalArticle

7 Citations (Scopus)
2011

Analysis and compression testing of laminates optimised for damage tolerance

Rhead, A. T., Butler, R. & Baker, N., Feb 2011, In : Applied Composite Materials. 18, 1, p. 85-100 16 p.

Research output: Contribution to journalArticle

File
28 Citations (Scopus)
139 Downloads (Pure)

Buckling and postbuckling of a delaminated composite beam in bending

Kinawy, M., Butler, R. & Hunt, G. W., Mar 2011, In : AIAA Journal. 49, 3, p. 670-672 3 p.

Research output: Contribution to journalArticle

7 Citations (Scopus)

Damage resistance and damage tolerance of hybrid carbon-glass laminates

Rhead, A. T., Shi, H. & Butler, R., 2011, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, AIAA 2011-2172

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Citations (Scopus)

Damage Resistance and Damage Tolerance of Hybrid Carbon-Glass Laminates

Rhead, A., Hua, S. & Butler, R., 11 Apr 2011. 12 p.

Research output: Contribution to conferencePaper

File
2 Citations (Scopus)
90 Downloads (Pure)

Maximizing compression after impact strength of uncoupled symmetric and non-symmetric laminates

Baker, N., Butler, R. & York, C. B., 2011, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics

Research output: Chapter in Book/Report/Conference proceedingConference contribution

The influence of fibre angle on the compressive strength of delaminated surface plies

Rhead, A., Butler, R. & Baker, N., 21 Aug 2011. 10 p.

Research output: Contribution to conferencePaper

File
2 Citations (Scopus)
36 Downloads (Pure)