Influence of cyclic stress intensity threshold on the scatter seen in cyclic Mode I fatigue delamination growth in DCB tests. (1st June 2017)
- Record Type:
- Journal Article
- Title:
- Influence of cyclic stress intensity threshold on the scatter seen in cyclic Mode I fatigue delamination growth in DCB tests. (1st June 2017)
- Main Title:
- Influence of cyclic stress intensity threshold on the scatter seen in cyclic Mode I fatigue delamination growth in DCB tests
- Authors:
- Mujtaba, A.
Stelzer, S.
Brunner, A.J.
Jones, R. - Abstract:
- Abstract: Whilst composite materials are now widely used in aircraft structural components for certification purposes current designs are such that any delamination/disbond will not grow. Despite this limit fleet data and data obtained from full scale fatigue tests reveal that small sub mm initial delaminations/disbonds can grow when subjected to operational flight loads. To account for this the US Federal Aviation Authority advisory circular AC20-107B outlines a slow growth approach for certifying composite/bonded aircraft structures. A key point in AC20-107B is that growth must be both slow and predictable. Since the life of an airframe is determined by the growth of the fastest (lead) crack/delamination/disbond any analysis tool developed for a composite/bonded airframe requires the ability to predict the both the scatter in delamination/disbond growth and thereby the growth of the lead delamination/disbond in the airframe. To this end the present paper reveals that the Hartman-Schijve variant of the NASGRO equation would appear to show promise for capturing the scatter seen in Mode I delamination tests associated with specimens fabricated from nominally identical material supplied by two different suppliers. It is shown that the values of the constants in the Hartman-Schijve equation associated with these two sources are consistent and the scatter in growth can captured by allowing for small variations in the fatigue threshold term.
- Is Part Of:
- Composite structures. Volume 169(2017)
- Journal:
- Composite structures
- Issue:
- Volume 169(2017)
- Issue Display:
- Volume 169, Issue 2017 (2017)
- Year:
- 2017
- Volume:
- 169
- Issue:
- 2017
- Issue Sort Value:
- 2017-0169-2017-0000
- Page Start:
- 138
- Page End:
- 143
- Publication Date:
- 2017-06-01
- Subjects:
- FAA AC20-107B -- Fatigue -- Delamination growth -- Scatter -- NASGRO
Composite construction -- Periodicals
Composites -- Périodiques
624.18 - Journal URLs:
- http://www.sciencedirect.com/science/journal/02638223 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.compstruct.2016.07.080 ↗
- Languages:
- English
- ISSNs:
- 0263-8223
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 3364.970000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 2714.xml