Zobrazeno 1 - 10
of 16
pro vyhledávání: '"N. F. Knight"'
Publikováno v:
Frattura ed Integrità Strutturale, Vol 5, Iss 15 (2013)
The Space Shuttle wing-leading edge consists of panels that are made of reinforced carbon-carbon. Coating spallation was observed near the slip-side region of the panels that experience extreme heating. To understand this phenomenon, a root-cause inv
Externí odkaz:
https://doaj.org/article/407abb3b76784f1cba5b04cd341c8013
Autor:
N. F. Knight
Publikováno v:
Academic Studies. Series “Pedagogy”. :23-28
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7c93a91cfbaca20bf69403f4d6dbe475
https://doi.org/10.52726/as.pedagogy/2022.3.4
https://doi.org/10.52726/as.pedagogy/2022.3.4
Autor:
N. F. Knight, M. V. Lukyanchuk
Publikováno v:
Academic Studies. Series “Pedagogy”. :64-73
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::92cbce2d4901b7c6055e5ba9c3f162b3
https://doi.org/10.52726/as.pedagogy/2021.2.10
https://doi.org/10.52726/as.pedagogy/2021.2.10
Autor:
N. F. Knight
Publikováno v:
AIAA Journal. 35:375-381
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e48901496a7be929d0d1ea31de9f0788
https://doi.org/10.2514/3.13513
https://doi.org/10.2514/3.13513
Autor:
N. F. Knight, W. S. Carron
Publikováno v:
AIAA Journal. 35:1876-1880
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a7e87fa5363ae18d9baf22c333216dc4
https://doi.org/10.2514/3.13764
https://doi.org/10.2514/3.13764
Publikováno v:
AIAA Journal. 30:2106-2113
A shear deformable (three-dimensional) shell element is used to analyze the panels. Two panels without boles and one with a bole are studied, and the resulting responses and failure modes comelated well with the experimental results.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::932f4623cbb852ec96b9d80221d5f6f2
https://doi.org/10.2514/3.11187
https://doi.org/10.2514/3.11187
Publikováno v:
32nd Structures, Structural Dynamics, and Materials Conference.
The objectives of the study are to assess the capability of a first-order shear deformable degenerated shell finite element theory to predict the postbuckling response and failure modes of various graphite-epoxy panels loaded in axial compression. Tw
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c7c9e75aaaa9fd32aa35d33ef5016754
https://doi.org/10.2514/6.1991-910
https://doi.org/10.2514/6.1991-910
Publikováno v:
31st Structures, Structural Dynamics and Materials Conference.
Advanced structural analysis and computational methods that exploit high-performance computers are being developed in a computational structural mechanics research activity sponsored by the NASA Langley Research Center. These new methods are develope
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::72fb2bd528778409b38e518df7939e89
https://doi.org/10.2514/6.1990-1145
https://doi.org/10.2514/6.1990-1145
Autor:
J. H. Starnes, N. F. Knight
Publikováno v:
Journal of Pressure Vessel Technology. 107:394-402
The results of an experimental and analytical study of the effects of circular holes on the postbuckling behavior of graphite-epoxy cylindrical panels loaded in axial compression are presented. The STAGSC-1 general shell analysis computer code develo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d8b34a6093a3b10b67721029f5b0b45
https://doi.org/10.1115/1.3264473
https://doi.org/10.1115/1.3264473
Publikováno v:
International Journal of Non-Linear Mechanics; 2002, Vol. 37 Issue: 4 p833-849, 17p