1. A critical review of available composite damage growth test data under fatigue loading and implications for aircraft sustainment. (15th January 2020) Authors: Molent, L.; Haddad, A. Journal: Composite structures Issue: Volume 232(2019) Page Start: Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
2. A review of equivalent pre‐crack sizes in aluminium alloy 7050‐T7451. (24th June 2014) Authors: Molent, L. Journal: Fatigue & fracture of engineering materials & structures Issue: Volume 37:Number 10(2014:Oct.) Page Start: 1055 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
3. A stress versus crack growth rate investigation (aka stress – cubed rule). (June 2016) Authors: Molent, L.; Jones, R. Journal: International journal of fatigue Issue: Volume 87(2016) Page Start: 435 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
4. A stress versus crack growth rate investigation (aka stress – cubed rule). (June 2016) Authors: Molent, L.; Jones, R. Journal: International journal of fatigue Issue: Volume 87(2016) Page Start: 435 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
5. A study of fatigue variability in aluminium alloy 7050-T7451. (November 2016) Authors: Dixon, B.; Molent, L.; Barter, S. Journal: International journal of fatigue Issue: Volume 92:Part 1(2016) Page Start: 130 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
6. Airframe metal fatigue revisited. (February 2020) Authors: Molent, L.; Dixon, B. Journal: International journal of fatigue Issue: Volume 131(2020) Page Start: Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
7. Alternative methods for derivation of safe life limits for a 7050-T7451 aluminium alloy structure. (May 2015) Authors: Molent, L. Journal: International journal of fatigue Issue: Volume 74(2015) Page Start: 55 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
8. Fatigue crack growth lessons from thirty-five years of the Royal Australian Air Force F/A-18 A/B Hornet Aircraft Structural Integrity Program. (April 2020) Authors: Main, B.; Molent, L.; Singh, R.; Barter, S. Journal: International journal of fatigue Issue: Volume 133(2020) Page Start: Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
9. Lessons from a fatigue prediction challenge for an aircraft wing shear tie post. (June 2019) Authors: Main, B.; Evans, R.; Walker, K.; Yu, X.; Molent, L. Journal: International journal of fatigue Issue: Volume 123(2019) Page Start: 53 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
10. Managing airframe fatigue from corrosion pits – A proposal. (March 2015) Authors: Molent, L. Journal: Engineering fracture mechanics Issue: Volume 137(2015) Page Start: 12 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗