Zobrazeno 1 - 10
of 38
pro vyhledávání: '"Yeong Moo Yi"'
Publikováno v:
Advanced Composite Materials. 23:43-52
Composite sandwich panels with face sheets made of carbon/epoxy fabric and carbon/epoxy uni-directional prepreg were tested. The sandwich cores made by aluminum honeycomb and foam were cured with t...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44689b1edb77e7b874c10b8cfc342dd2
https://doi.org/10.1080/09243046.2013.862386
https://doi.org/10.1080/09243046.2013.862386
Publikováno v:
Key Engineering Materials. 433:219-224
In this paper, mould configurations are studied by finite element simulation for superplastic blow forming of combustion chamber outer jacket. One concave and two convex mould configurations are basically considered to determine which type would be a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::53696ae982d3e2cdd205af37a087ee01
https://doi.org/10.4028/www.scientific.net/kem.433.219
https://doi.org/10.4028/www.scientific.net/kem.433.219
Publikováno v:
Key Engineering Materials. 433:57-62
Titanium alloys have been widely used in aeronautics and aerospace industries due to their high strength, good corrosion resistance and low density. Since many aerospace vehicle systems require high performance lightweight pressurized vessel for stor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64189148283bced7081e7a3373b9e298
https://doi.org/10.4028/www.scientific.net/kem.433.57
https://doi.org/10.4028/www.scientific.net/kem.433.57
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 38:29-34
*O UIJT TUVEZ KPJOU TUSFOHUI BOE GBJMVSF DIBSBDUFSJTUJDT XFSF FYQFSJNFOUBMMZ FYBNJOFEXJUI QVMM PVU BOE TIFBS TQFDJNFOT JO XIJDI OFX EFTJHOFE IJHI T USFOHUI JOTFSU XBTBQQMJFE 5IFQFSGPSNBODFPGUIFOFXJOTFSUXBTDPNQBSFEXJUIUZQJDBM JOTFSU EFTJHO 5IF FYQFSJN
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8dfe17c5ed2760ce1df10deb7095e71d
https://doi.org/10.5139/jksas.2010.38.1.029
https://doi.org/10.5139/jksas.2010.38.1.029
Publikováno v:
SAE International Journal of Aerospace. 2:258-262
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::50e46656d855d3942b90620cf1bfd6ba
https://doi.org/10.4271/2009-01-3259
https://doi.org/10.4271/2009-01-3259
Publikováno v:
Thermochimica Acta. 494:123-128
Accepted: 2009-05-01
資料番号: SA1000901000
資料番号: SA1000901000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8df7a824657c5c85f6eec46e5c0117f1
https://doi.org/10.1016/j.tca.2009.05.002
https://doi.org/10.1016/j.tca.2009.05.002
Publikováno v:
Journal of Materials Processing Technology. 201:280-284
Massive diffusion bonding (MDB) is an innovative manufacturing method to produce heavy titanium parts with solid-state bonding of multi-sheets by applying low pressure of inert gas. Massive solid-state bonding is different from conventional diffusion
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df58dea6c3e917b7d3085c5690ae91fc
https://doi.org/10.1016/j.jmatprotec.2007.11.183
https://doi.org/10.1016/j.jmatprotec.2007.11.183
Publikováno v:
Advanced Materials Research. :359-362
It is well known that the utilization of superplastic characteristics in manufacturing process makes many of aerospace components lighter and stiffer. The weight saving is vitally important especially for aerospace application and even more weight sa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b9adf25357baf69ec6fd6194a9697ca
https://doi.org/10.4028/www.scientific.net/amr.26-28.359
https://doi.org/10.4028/www.scientific.net/amr.26-28.359
Autor:
Young-Soon Jang, Jong Woong Lee, Se Won Eun, Gwang Rae Cho, Yeong Moo Yi, Jae Sung Park, Cheol Won Kong
Publikováno v:
Key Engineering Materials. :605-608
Composite materials are used in aerospace structures due to their considerable bending stiffness and strength-to-weight ratio. A composite sandwich is composed of a face-sheet and an aluminum core. The face-sheet of the sandwich takes the bending str
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4cd462542f76b69b9164912d30bfd09b
https://doi.org/10.4028/www.scientific.net/kem.348-349.605
https://doi.org/10.4028/www.scientific.net/kem.348-349.605
Publikováno v:
Key Engineering Materials. :549-552
It is known that Ti-6Al-4V alloy is one of the excellent candidates for aerospace structure due to their high specific strength.However, its higher cost and low formability relative to other materials tend to limit the wide usage of the material.The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7183f79d7226d67e0292cab10a061215
https://doi.org/10.4028/www.scientific.net/kem.345-346.549
https://doi.org/10.4028/www.scientific.net/kem.345-346.549