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25篇 您的检索式：作者名="NABOULSI S"

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	题名	作者	年代	出处	被引量
1	Fretting Fatigue Crack Initiation Behavior Using Process Volume Approach and Finite Ele- ment Analysis 显示文摘	NABOULSI S MALL S	2003	Tribology International2003，36，：	1
2	Characterization of fatigue crack growth in aluminum panels with a bonded composite patch 显示文摘	NABOULSI S MALL S	1997	Composite Structure1997，37，34：	1
3	Investigation of geometric imperfection in inflatable aerospace structures 显示文摘	NABOULSI S	2004	Journal of Aerospace Engineering2004，17，3：	1
4	Thermal effects on adhesively bonded composite repair of cracked aluminum panels显示文摘	Mall S	1997	Theoretical and Applied Fracture Mechanics1997，7478，：	1
5	Thermal effects on adhesively bonded composite repair of cracked aluminum panels显示文摘	Naboulsi S Mall S	1997	Theoretical Applied Fracture Mechanics1997，26，：	1
6	Modeling of a cracked metallic structure with bonded composite patch using the three layer technique显示文摘	Mall S Naboulsi S	1996	Composite Structures1996，35，3：	1
7	Modeling of cracked metallic structure with bonded composite path using three layer technique显示文摘	Naboulsi S Mall S	1996	Composite Structure1996，35，2：	1
8	Nonlinear analysis of bonded composite patch repair of cracked aluminum panels显示文摘	Naboulsi S Mall S	1998	Composite Structures1998，41，34：	1
9	Thermal effects on adhesively bonded composite repair of cracked aluminum panels显示文摘	Naboulsi S Mall S	1997	Theoretical and Applied Fracture Mechanics1997，26，1：	1
10	Investigation of geometric imperfection in inflatable aerospace structures 显示文摘	NABOULSI S	2004	Journal of Aerospace Engineering2004，17，3：	1
11	Investigation of geometric imperfection in inflatable aerospace structures显示文摘		2004	Journal of Aerospace Engineering2004，17，3：	1
12	Application of crack analogy to fretting fatigue显示文摘	Naboulsi S	2005	Engineering Fracture Mechanics2005，72，10：	1
13	Investigation of geometric imperfection ininflatable aerospace structures显示文摘	Naboulsi S	2004	Journal of AerospaceEngineering2004，17，3：	1
14	Application of crack analogy to fretting fatigue 显示文摘	Naboulsi S	2005	Engineering Fracture Mechanics2005，72，12：	1
15	Thermal effects on adhesively bonded composite repair of cracked aluminum panels显示文摘	Naboulsi S Mall S	1997	Theoretical and Applied Fracture Mechanics1997，26，：	1
16	Thermal Effects on Adhesively Bonded Composite Repair of Cracked Aluminum Panels显示文摘	NABOULSI S MALL S	1997	Theoretical and Applied Fracture Mechanics1997，，26：	1
17	Investigation of geometric imperfection in inflatable aerospace structures 显示文摘	Naboulsi S	2004	Journal of Aerospace Engineering2004，17，3：	1
18	Modeling of a cracked metallic structure with bonded composite patch using the three layer technique 显示文摘	S Naboulsi	1995	Composite Structures1995，，35：	1
19	Nonlinear analysis of bonded composite patch repair of cracked aluminum panels 显示文摘	Naboulsi S Mall S	1998	Compos Struct1998，，41：	1
20	Modeling of cracked metallic structure with bonded composite patch using three lay- er technique显示文摘	Naboulsi S Mall S	1996	Composite Structure1996，35，3：	1

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