Wang, J.T., Jegley, D.C., Bush, H.G. and Hinrichs, S.C., "Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box," NASA TM-110267, 1996. Home/Search Document Not in Database Summary Related Articles Check |
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, was shown to decrease once the debond had grown beyond the.. - Continued To Be (1998) (Correct)
....stitched to the skin. Once the preform is assembled, resin film infusion (RFI) is used to impregnate the entire structure with epoxy resin [1] Skin stiffener interface stresses may be large enough to cause a separation between the skin and stiffening elements resulting in a delamination or debond [2]. The effects of stitching on delamination or debond growth in composites have been examined in simple two and three dimensional configurations by modeling the stitches as truss or beam elements connecting nodes through the thickness of the material [3 5] An advantage of the three dimensional ....
Wang, J.T., Jegley, D.C., Bush, H.G. and Hinrichs, S.C., ÒCorrelation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box,Ó NASA TM-110267, 1996.
Application of Interface Technology in Nonlinear Analysis of a .. - Wang, Ransom (1997) (1 citation) Self-citation (Wang) (Correct)
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Wang, J. T., Jegley, D. C., Bush, H. G., and Hinrichs, S. C., Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box, NASA TM-110267, July 1996.
Modeling The Influence Of Stitching - On Delamination Growth (1999) (Correct)
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Wang, J.T., Jegley, D.C., Bush, H.G. and Hinrichs, S.C., "Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box," NASA TM-110267, 1996.
Research and Applications in Structures at the NASA Langley.. - Abel (1997) (Correct)
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Wang, J. T.; Jegley, D. C.; Bush, H. G.; and Hinrichs, S. C.: Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box. NASA TM-110267, July 1996.
Modeling The Influence Of Stitching On Delamination Growth.. - Glaessgen Raju And (1999) (Correct)
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Wang, J.T., Jegley, D.C., Bush, H.G. and Hinrichs, S.C., ÒCorrelation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box,Ó NASA TM-110267, 1996.
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