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29篇 您的检索式：作者名="BELLINGER N C"

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	题名	作者	年代	出处	被引量
1	Effects of Ultrasonic Impact Treatment on Fatigue Behavior of Naturally Exfoliated Aluminum Al- loys 显示文摘	Liao M Chen W R Bellinger N C	2008	International journal of Fatigue2008，30，4：	1
2	Study of the residual strain in lap joints显示文摘	LI G SHI G Q BELLINGER N C	2006	Journal of Aircraft2006，43，4：	1
3	Residual Life Predictions of Corroded Fuselage Lap Joints显示文摘	BELLINGER N C KOMOROWSKI J P BENAK T J	2001	International Journal of Fatigue2001，23，：	1
4	Damage tolerance based life prediction of aeroengine compressor disk: a deterministic fracture mechanics approach 显示文摘	Koul A K Bellinger N C Fahr A	1990	International Journal of Fatigue1990，5，：	1
5	Modeling the Effects of Prior Exfoliation Corrosion on Fatigue Life of Aircraft Wing Skins显示文摘	LIAO Min BELLINGEr N C KOMOROWSKI J P	2003	International Journal of Fatigue2003，25，12：	1
6	Residual life predictions of corroded fuselage lap joints显示文摘	Bellinger N C Komorowski J P and Benak T J	2001	International Journal of Fatigue2001，23，1：	1
7	Impulse Buying Varies by Product 显示文摘	Bellinger D N Robertson D H Hirschman E C	1978	Journal of Advertising Research1978，18，：	1
8	Residual life predictions of corroded fuselage lap joints显示文摘	Bellinger N C Komorowski J P Benak T J	2001	International Journal of Fatigue2001，23，1：	1
9	Damage-tolerance-based life prediction of aeroengine compressor discs: I a deter- ministic fracture mechanics approach 显示文摘	Koul A K Bellinger N C Fahr A	1990	International Journal of Fatigue1990，12，5：	1
10	Selecting representative reserve systems in remote areas:A case study in the Nullarbor region,Australia显示文摘	MeKenzie N L Belling L Margules C R		0，，1：	1
11	Effects of ultrasonic im- pact treatment on fatigue behavior of naturally exfoliated a- luminum alloys显示文摘	Liao M Chen W R Bellinger N C	2008	Int J Fatigue2008，30，4：	1
12	Studies of residual stress in sin- gle-Row countersunk riveted lap joints显示文摘	Li G Shi G Q Bellinger N C	2006	Journal of Aircraft2006，43，3：	1
13	Residual life predictions of corroded fuselage lap joints 显示文摘	Bellinger N C Komorowski J P Benak T J	2001	International Journal of Fatigue2001，23，1：	1
14	Residual life predictions of corroded fuselage lap joints显示文摘	Bellinger N C Komorowski J P Benak T J	2001	International Journal of Fatigue2001，23，1：	1
15	Corrosion PillowingStresses in Fuselage Lap Joints显示文摘	BELLINGER N C KOMOROWSKI J P	1997	AIAA Journal1997，35，2：	1
16	Corrosion pillowing stresses in fuselage lapped plates显示文摘	BELLINGER N C KOMOROWSKI P J	1997	AIAA J1997，35，3：	1
17	Fatigue modeling for aircraft structures containing natural exfoliation corrosion显示文摘	LIAO M RWNAUD G BELLINGER N C	2007	International Journal of Fatigue2007，29，：	1
18	Damage tolerance implications of corrosion pillowing on fuselage lapped plates显示文摘	BELLINGER N C KOMOROWSKI J P GOULD R W	1998	J Aircraft1998，35，3：	1
19	Effects of ultrasonic impact treatment on fatigue behavior of naturally exfoliated aluminum alloys显示文摘	LIAO M CHEN W R BELLINGER N C	2008	International Journal of Fatigue2008，30，4：	1
20	Fatigue Modeling for Aircraft Structures Containing Natural Exfoliation Corro- sion 显示文摘	Liao M Renaud G Bellinger N C	2007	International Journal of Fatigue2007，29，4：	1

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