The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength

Original language	English
Publication status	Published - 2016
Event	5th Aircraft Structural Design Conference - Manchester, United Kingdom Duration: 04 Oct 2016 → 06 Oct 2016

Conference

Conference	5th Aircraft Structural Design Conference
Country/Territory	United Kingdom
City	Manchester
Period	04/10/2016 → 06/10/2016

Student theses

• Simulation intent for multi-fidelity composite structural analysis

  Harley, C. (Author), Robinson, T. (Supervisor), Quinn, D. (Supervisor) & Nolan, D. (Supervisor), Jul 2021

  Student thesis: Doctoral Thesis › Doctor of Philosophy

  File

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Harley, C., Quinn, D., Robinson, T., & Goel, S. (2016). The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength. Paper presented at 5th Aircraft Structural Design Conference, Manchester, United Kingdom.

Harley, Cara ; Quinn, Damian ; Robinson, Trevor et al. / The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength. Paper presented at 5th Aircraft Structural Design Conference, Manchester, United Kingdom.

@conference{2cf1fb38999c4a26b83113cb1ef8b47f,

title = "The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength",

author = "Cara Harley and Damian Quinn and Trevor Robinson and Saurav Goel",

year = "2016",

language = "English",

note = "5th Aircraft Structural Design Conference ; Conference date: 04-10-2016 Through 06-10-2016",

}

Harley, C, Quinn, D, Robinson, T & Goel, S 2016, 'The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength', Paper presented at 5th Aircraft Structural Design Conference, Manchester, United Kingdom, 04/10/2016 - 06/10/2016.

The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength. / Harley, Cara; Quinn, Damian; Robinson, Trevor et al.
2016. Paper presented at 5th Aircraft Structural Design Conference, Manchester, United Kingdom.

Research output: Contribution to conference › Paper › peer-review

TY - CONF

T1 - The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength

AU - Harley, Cara

AU - Quinn, Damian

AU - Robinson, Trevor

AU - Goel, Saurav

PY - 2016

Y1 - 2016

M3 - Paper

T2 - 5th Aircraft Structural Design Conference

Y2 - 4 October 2016 through 6 October 2016

ER -

Harley C, Quinn D, Robinson T, Goel S. The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength. 2016. Paper presented at 5th Aircraft Structural Design Conference, Manchester, United Kingdom.