Zobrazeno 1 - 10
of 25
pro vyhledávání: '"A. F. Grandt"'
Purdue University has played a leading role in providing the engineers who designed, built, tested, and flew the many aircraft and spacecraft that so changed human progress during the 20th century. It is estimated that Purdue has awarded 6% of all BS
Publikováno v:
One Small Step
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44ea31312eb0da3caca7877c7137902c
https://doi.org/10.2307/j.ctv15wxp00.5
https://doi.org/10.2307/j.ctv15wxp00.5
Publikováno v:
One Small Step
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f43236c8e3182a5feda916810699c507
https://doi.org/10.2307/j.ctv15wxp00.4
https://doi.org/10.2307/j.ctv15wxp00.4
Autor:
F. Grandt
Publikováno v:
Procedia Engineering. 17:236-246
Damage tolerant design and nondestructive inspection are key tasks for ensuring aircraft airworthiness. Damage tolerance is the ability to resist fracture from preexistent damage for a given period of time and is an essential attribute of components
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::06440acd30f3e5e0c89bdc253aa4d2eb
https://doi.org/10.1016/j.proeng.2011.10.025
https://doi.org/10.1016/j.proeng.2011.10.025
Publikováno v:
Journal of Manufacturing Science and Engineering. 124:809-819
It is well known that there is a large variance associated with fatigue life. However, in literature little is found on the relationship between manufacturing processes and fatigue variance of the manufactured components. In this research, the influe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c5f7fa8eb07b9cc925091b314a6efa6
https://doi.org/10.1115/1.1511174
https://doi.org/10.1115/1.1511174
Autor:
J. N. Scheuring, A. F. Grandt
Publikováno v:
Journal of Engineering Materials and Technology. 119:380-386
This paper evaluates changes in the behavior of aircraft materials which result from aging and/or corrosion that occurs during long periods of service usage. The primary objective was to determine whether damage tolerant analyses for older aircraft s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::639b274f4ba5969cf39ea988c4e1e3f5
https://doi.org/10.1115/1.2812273
https://doi.org/10.1115/1.2812273
Publikováno v:
Metallurgical and Materials Transactions A. 28:1157-1167
Fatigue initiation lifetimes were demonstrated to be related to the size and density of microporosity in the midplate region for three differently processed variations of aluminum alloy 7050-T7451. Metallographic and fractographic examination of doub
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::40c28313473aa781a6186fa73fa9841c
https://doi.org/10.1007/s11661-997-0281-5
https://doi.org/10.1007/s11661-997-0281-5
Publikováno v:
Journal of Aircraft. 33:1003-1013
This article describes research aimed at predicting the fatigue lives of unstiffened aluminum panels that contain multiple site damage (MSD). The initial damage consists of through-the-thickness cracks emanating from a row of holes in the center of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75a42666dc27e97b54bf48abfdd63c4d
https://doi.org/10.2514/3.47047
https://doi.org/10.2514/3.47047
Publikováno v:
Journal of Aircraft. 33:1014-1021
This article describes research aimed at predicting the residual strength (RS) of unstiffened aluminum panels that contain multiple site damage (MSD). The initial damage consists of through-the-t hickness cracks emanating from a row of holes in the c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::11e0079908eb9a5a85ca4997e4a78067
https://doi.org/10.2514/3.47048
https://doi.org/10.2514/3.47048