L. Molent - Publications, H-index & Citations

L. Molent

molent aerostructures

31H指数

108论文数

2.6K被引数

收录论文 38

发表时间

Effect of laser heat treatment on fatigue crack growth in AA2198-T851 thin sheets under constant-amplitude and spectrum loadings 激光热处理对AA2198-T851薄板在恒幅和谱载荷下疲劳裂纹扩展的影响

materials science and engineering: a

IF0

2026-05-30

OAAI

C.P. Carvalho; J.P. Pascon; M.S.F. Lima; L. Molent; C.A.R.P. Baptista

Crack-like effectiveness of some discontinuities in AA2024

FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES

IF3.2

2023-09-07

OAAI

Molent, Loris; Fox, Matthew R.

Fatigue crack growth lessons from thirty-five years of the Royal Australian Air Force F/A-18 A/B Hornet Aircraft Structural Integrity Program

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2020-04-01

PREAI

Main, B.; Molent, L.; Singh, R.; Barter, S.

Airframe metal fatigue revisited

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2020-02-01

PREAI

Molent, L.; Dixon, B.

A critical review of available composite damage growth test data under fatigue loading and implications for aircraft sustainment

COMPOSITE STRUCTURES

IF7.1

2020-01-01

PREAI

Molent, L.; Haddad, A.

Lessons from a fatigue prediction challenge for an aircraft wing shear tie post

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2019-06-01

PREAI

Main, B.; Evans, R.; Walker, K.; Yu, X.; Molent, L.

Outcomes from the fatigue testing of seventeen centre fuselage structures

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2018-06-01

PREAI

Molent, L.; Barter, S. A.; Dixon, B.; Swanton, G.

Using the lead crack concept and fractal geometry for fatigue lifing of metallic structural components

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2017-09-01

PREAI

Molent, Loris; Spagnoli, Andrea; Carpinteri, Andrea; Jones, Rhys

The lead crack concept applied to defect growth in aircraft composite structures

COMPOSITE STRUCTURES

IF7.1

2017-04-01

PREAI

Molent, L.; Forrester, C.

A study of fatigue variability in aluminium alloy 7050-T7451

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2016-11-01

PREAI

Dixon, B.; Molent, L.; Barter, S.

A stress versus crack growth rate investigation (aka stress - cubed rule)

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2016-06-01

PREAI

Molent, L.; Jones, R.

The influence of cyclic stress intensity threshold on fatigue life scatter

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2016-01-01

PREAI

Molent, L.; Jones, R.

The equivalence of EPS and EIFS based on the same crack growth life data

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2015-11-01

PREAI

Gallagher, J. P.; Molent, L.

Alternative methods for derivation of safe life limits for a 7050-T7451 aluminium alloy structure

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2015-05-01

PREAI

Molent, L.

Supersonic particle deposition as a means for enhancing the structural integrity of aircraft structures

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2014-11-01

PREAI

Jones, R.; Molent, L.; Barter, S.; Matthews, N.; Tamboli, D.

A review of equivalent pre-crack sizes in aluminium alloy 7050-T7451

FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES

IF3.2

2014-06-24

PREAI

Molent, L.

Calculating crack growth from small discontinuities in 7050-T7451 under combat aircraft spectra

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2013-10-01

PREAI

Jones, R.; Molent, L.; Barter, S. A.

Verification of an individual aircraft fatigue monitoring system

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2012-10-01

PREAI

Molent, L.; Barter, S.; Foster, W.

Typical fatigue-initiating discontinuities in metallic aircraft structures

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2012-08-01

PREAI

Barter, S. A.; Molent, L.; Wanhill, R. J. H.

Fatigue crack growth in a diverse range of materials

INTERNATIONAL JOURNAL OF FATIGUE

IF6.8

2012-07-01

PREAI

Jones, R.; Molent, L.; Walker, K.

研究方向