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X
Ratwani, M. M.
~ 200  Ergebnisse:
Personensuche X
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1

Effects of composite adherend properties on stresses in dou..:

Mokhtari, M. ; Madani, K. ; Belhouari, M....
Materials & Design.  44 (2013)  - p. 633-639 , 2013
Link: https://doi.org/10.1016/..
 
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2

Experimental and numerical study of repair techniques for p..:

Madani, K. ; Touzain, S. ; Feaugas, X...
Computational Materials Science.  48 (2010)  1 - p. 83-93 , 2010
Link: https://doi.org/10.1016/..
 
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3

Stress distribution in a 2024-T3 aluminum plate with a circ..:

Madani, K. ; Touzain, S. ; Feaugas, X...
International Journal of Adhesion and Adhesives.  29 (2009)  3 - p. 225-233 , 2009
Link: https://doi.org/10.1016/..
 
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4

Numerical analysis for the determination of the stress inte..:

Madani, K. ; Touzain, S. ; Feaugas, X...
Computational Materials Science.  42 (2008)  3 - p. 385-393 , 2008
Link: https://doi.org/10.1016/..
 
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5

Crack opening displacement in plate with bonded repair patc:

RATWANI, M. M. ; KIEBOOM, O. T. ; HESLEHURST, R. B.
FatigueFracture of Engineering Materials and Structures.  29 (2006)  6 - p. 425-430 , 2006
Link: https://doi.org/10.1111/..
 
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6

Case HistoryComposite Patch Reinforcement of T-38 Lower Win..:

, In: Advances in the Bonded Composite Repair of Metallic Aircraft Structure,
RATWANI, M ; HELBLING, J ; HEIMERDINGER, B. - p. 997-1008 , 2002
Link: https://doi.org/10.1016/..
 
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7

Analysis of composite-to-metal joints with bondline flaws:

Ratwani, M.M. ; Kan, H.P.
Composites Science and Technology.  23 (1985)  1 - p. 53-72 , 1985
Link: https://doi.org/10.1016/..
 
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8

Stress analysis of stepped-lap joints with bondline flaws:

Kan, H. P. ; Ratwani, M. M.
Journal of Aircraft.  20 (1983)  10 - p. 848-852 , 1983
Link: https://doi.org/10.2514/..
 
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9

Time-dependent adhesive behavior effects in a stepped lap j..:

Ratwani, M. M. ; Kan, H. P. ; Liu, D. D.
AIAA Journal.  20 (1982)  5 - p. 734-736 , 1982
Link: https://doi.org/10.2514/..
 
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10

Nonlinear adhesive behavior effects in cracked metal-to-com..:

Kan, H.P. ; Ratwani, M.M.
Engineering Fracture Mechanics.  15 (1981)  1-2 - p. 123-130 , 1981
Link: https://doi.org/10.1016/..
 
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11

Fatigue crack growth at stress concentrations subjected to ..:

Ratwani, M. ; Wilhem, D. P. ; Carter, J. P...
Journal of Aircraft.  18 (1981)  3 - p. 206-212 , 1981
Link: https://doi.org/10.2514/..
 
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12

Compression Fatigue Analysis of Fiber Composites:

Ratwani, M.M. ; Kan, H.P.
Journal of Aircraft.  18 (1981)  6 - p. 458-462 , 1981
Link: https://doi.org/10.2514/..
 
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13

Influence of nonlinear adhesive behavior on analysis of cra..:

Ratwani, M. M. ; Kan, H. P.
AIAA Journal.  18 (1980)  10 - p. 1275-1278 , 1980
Link: https://doi.org/10.2514/..
 
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14

Analysis of Cracked, Adhesively Bonded Laminated Structures:

Ratwani, M.M.
AIAA Journal.  17 (1979)  9 - p. 988-994 , 1979
Link: https://doi.org/10.2514/..
 
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15

Influence of biaxial loading on analysis of cracked stiffen..:

Ratwani, M.M. ; Wilhem, D.P.
Engineering Fracture Mechanics.  11 (1979)  3 - p. 585-593 , 1979
Link: https://doi.org/10.1016/..
 
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