Zobrazeno 1 - 10
of 20
pro vyhledávání: '"C Penmetsa"'
Publikováno v:
Journal of Engineering Materials and Technology. 140
Next-generation, reusable hypersonic aircraft will be subjected to extreme environments that produce complex fatigue loads at high temperatures, reminiscent of the life-limiting thermal and mechanical loads present in large gas-powered land-based tur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de51053b47201059af1229a425cc23c9
https://doi.org/10.1115/1.4040223
https://doi.org/10.1115/1.4040223
Publikováno v:
Composite Structures. 102:38-60
Delamination between plies is the most common failure mode in composite laminates that can cause fiber breakage and reduction in life of the composite. Currently Mode-I interlaminar fracture toughness or critical energy release rate of a composite is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8da628e13af0a4d29f530c8a06e69529
https://doi.org/10.1016/j.compstruct.2013.01.020
https://doi.org/10.1016/j.compstruct.2013.01.020
Publikováno v:
18th AIAA Non-Deterministic Approaches Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b182caa0e214b820609a847cd44f0421
https://doi.org/10.2514/6.2016-0428
https://doi.org/10.2514/6.2016-0428
Publikováno v:
Fatigue & Fracture of Engineering Materials & Structures. 35:328-346
In the recent years, Cohesive Zone Models (CZMs) have gained increasing popularity for modelling the fracture process [1] and also in other applications like composite de-lamination [2] solder failures [3] in circuits, etc. This can be attributed to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5cada7c1203d92f40634c8a92ba02d56
https://doi.org/10.1111/j.1460-2695.2011.01624.x
https://doi.org/10.1111/j.1460-2695.2011.01624.x
Publikováno v:
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Cumulative damage theory has been extended to develop a deterministic fatigue life prediction model for materials subjected to superimposed thermo-acousto-mechanical cycling. This loading profile is exhibited by particular external panels of reusable
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c2c8a93bf9fb98f0b77ef4aabbe4404e
https://doi.org/10.2514/6.2015-1580
https://doi.org/10.2514/6.2015-1580
Publikováno v:
17th AIAA Non-Deterministic Approaches Conference.
To alleviate computational challenges in uncertainty quantification and multidisciplinary design optimization, Kriging has gained its popularity due to its high accuracy and flexibility interpolating non-linear system responses with collected data. O
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::545e5214031faf17ededa53707b7ae30
https://doi.org/10.2514/6.2015-1372
https://doi.org/10.2514/6.2015-1372
Publikováno v:
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
In light of the combined extreme environment to which hypersonic fuselage components will be subjected, a unique test platform has been developed for evaluating materials and structures under service-like conditions. Typical ascent-cruise-descent mis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c16998411a9282e084d74e5e59ad2a4b
https://doi.org/10.2514/6.2015-1434
https://doi.org/10.2514/6.2015-1434
Publikováno v:
16th AIAA Non-Deterministic Approaches Conference.
A structural hot spot was traditionally reserved to represent a region of high stress that has a high probability for premature fatigue damage. However, in this research hot spot is defined as a location that might have high probability-of-failure or
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8655c5c0edc409f01bd07372ab2fe5b
https://doi.org/10.2514/6.2014-0644
https://doi.org/10.2514/6.2014-0644
Publikováno v:
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
When testing for material properties, the cost and time of the tests are an important factor. It is not practical to test every possible combination of expected environmental and loading scenarios. Therefore, a set of limited data is collected based
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4b707f2965fda904f9d27366464ff56a
https://doi.org/10.2514/6.2013-1817
https://doi.org/10.2514/6.2013-1817
Publikováno v:
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference20th AIAA/ASME/AHS Adaptive Structures Conference14th AIAA.
Delamination between plies is the most common failure mode in composite laminates that can cause ber breakage and reduction in life of the composite. Currently Mode-I interlaminar fracture toughness or critical energy release rate of a composite is m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bfc1ff000b9a73e8df2c74f671480e4
https://doi.org/10.2514/6.2012-1940
https://doi.org/10.2514/6.2012-1940