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43篇 您的检索式：作者名="Molent"

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	题名	作者	年代	出处	被引量
1	Study of Multi-site Damage of Fuselage Lap Joints显示文摘	JONES R MOLENT L PITT S	1999	Theoretical and Applied Fracture Mechanics1999，32，1：	1
2	Study of multi- site damage of fuselage -lap joints 显示文摘	Jones R Molent L Pitt S	1999	Theoretical and Applied Fracture Mechanics1999，32，1：	1
3	Application of constitutive modeling and advanced repair technology to F-111C aircraft显示文摘	Molent L	2004	Composite Structures2004，66，：	1
4	An equivalent block method for computing fatigue crack growth显示文摘	JONES R MOLENT L KRISHNAPILLAI K	2008	International Journal of Fatigue2008，30，：	1
5	An experimental evaluation of fatigue crack growth显示文摘	Barter S Molent L Goldsmith N	2005	Engineering Failure Analysis2005，，12：	1
6	Understanding crack growth in fuselage lap joints显示文摘	Jones R Molent L Pitt S	2008	Theoretical andApplied Fracture Mechanics2008，49，1：	1
7	An equivalent block method for computing fatigue crack growth 显示文摘	Jones R Molent L Krishnapillai K	2008	International Journal of Fatigue2008，30，9：	1
8	Understanding crack growth in fuselage lap joints显示文摘	Jones R Molent L Pitt S	2008	Theoretical and Applied Fracture Mechanics2008，49，1：	1
9	A comparison of crack growth be- havior in several full-scale airframe fatigue tests显示文摘	Molent L Barter S A	2007	Inter- national Journal of Fatigue2007，29，6：	1
10	Typical fa-tigue-initiating discontinuities in metallic aircraft structures显示文摘	BARTER S A MOLENT U WANHILL R J H	2012	International Journal of Fatigue2012，41，3：	1
11	Clinical signs and performance of pigs treated with different doses of carbadox,cyadox and olaquindox显示文摘	NABUURS M J A MOLENT E J GRAAF G J	1990	J Vet Med1990，387，：	1
12	Interpreting fatigue test results using a probabilistic fracture approach 显示文摘	WHITE P MOLENT L Barter S	2005	Interna- tional Journal of Fatigue2005，27，7：	1
13	Characterisation of e-quivalent initial flaw sizes in 7050 aluminium alloy 显示文摘	MOLENT L SUN Q GREEN A J	2006	Fatigue and Fracture of Engineering Materials and Struc- tures2006，29，11：	1
14	Recent develop ments in fatigue crack growth assessment显示文摘	MOLENT L JONES R BARTER S	2006	International Journal of Fatigue2006，28，12：	1
15	Observations of Crack Path Changes Caused by Periodic Underloads in AA7050-T7451 显示文摘	White P Barter S A Molent L	2008	International Journal of Fatigue2008，30，7：	1
16	On the Glinka and Neuber methods for calculating notch tip strains under cyclic load spectra显示文摘	Knop M Jones R Molent L	2000	International Journal of Fatigue2000，22，：	1
17	Characterisation of equivalent initial flaw sizes in 7050 aluminium alloy显示文摘	MOLENT L SUN Q GREEN A J	2006	Fatigue & Fracture of Engineering Materials & Structures2006，29，11：	1
18	On the Glinka and Neuber methods for calculating notch tip strains under cyclic load spectra显示文摘	M Knop R Jones L Molent C Wang	2000	International Journal of Fatigue2000，，9：	1
19	Study of multi-site damage of fuselage lap joints显示文摘	JONES R MOLENT L PITT S	1999	Theoretical and Applied Fracture Mechanics1999，32，2：	1
20	Typical fa- tigue-initiating discontinuities in metallic aircraft structures 显示文摘	BARTER S A MOLENT L WANHILL R J H	2012	International Journal of Fatigue2012，41，：	1

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