Zobrazeno 1 - 10
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pro vyhledávání: '"S. Talya"'
Akademický článek
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Publikováno v:
Powder Technology. 394:1186-1194
Direct impingement (DI) erosion testing of steel and cobalt-based alloys is conducted with particles entrained in air and water. The tests are performed using 75- and 300-μm silica particles with three particle velocities and five impact angles. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1adfd9318e8db752120c603035bc1ad
https://doi.org/10.1016/j.powtec.2021.09.057
https://doi.org/10.1016/j.powtec.2021.09.057
Publikováno v:
Concurrent Engineering. 16:139-147
This study presents an application of a distributed service-oriented architecture (FIPER) for the preliminary design of gas turbines. The FIPER architecture is based on the concept of registration and discovery of services in real time. It uses a ser
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8f66a252224fa93cb0b7e5ba296e66dd
https://doi.org/10.1177/1063293x08092487
https://doi.org/10.1177/1063293x08092487
Publikováno v:
Engineering Optimization. 34:175-194
A multidisciplinary optimization procedure for gas turbine blade design has been developed and demonstrated on a generic 3-D blade. The blade is cooled both internally and externally (film cooling). Aerodynamic and heat transfer design criteria are i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff0a18db065bf0f80ae56f2527ea6a03
https://doi.org/10.1080/03052150210917
https://doi.org/10.1080/03052150210917
Publikováno v:
Inverse Problems in Engineering. 8:283-308
A multidisciplinary optimization procedure for gas turbine airfoil design has been developed and demonstrated on a generic blade. Aerodynamic and heat transfer design objectives are integrated along with various constraints on the airfoil geometry. H
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0a74ac878ec243bbb234a37d8a9297f4
https://doi.org/10.1080/174159700088027731
https://doi.org/10.1080/174159700088027731
Publikováno v:
Mathematical Problems in Engineering, Vol 5, Iss 2, Pp 97-119 (1999)
Design optimization of a gas turbine blade geometry for effective film cooling toreduce the blade temperature has been done using a multiobjective optimization formulation. Three optimization formulations have been used. In the first, the average bla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a92faf81ab32c5366718e2be7c7aaf4a
https://doaj.org/article/00ae95a81424480b8d463650a3ca7cc7
https://doaj.org/article/00ae95a81424480b8d463650a3ca7cc7
A Robust & Secure System for Performing Engineering Analysis and Design in a Distributed Environment
Publikováno v:
45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference.
In today's fast paced economy product design is becoming increasingly complex and requires tighter integration of the engineering and business processes not only within the individual businesses, but also across enterprises. This high demand for real
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dfbd31c35b7bcd325b42414914e05879
https://doi.org/10.2514/6.2004-1847
https://doi.org/10.2514/6.2004-1847
Akademický článek
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Publikováno v:
8th Symposium on Multidisciplinary Analysis and Optimization.
A multidisciplin ary design optimization procedure for gas turbine blade design has been developed and demonstrated on a generic 3-D blade. Aerodynamic, heat transfer, structural and modal design objectives are integrated along with various constrain
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::538b623ae35515c2b774fc8a53539a73
https://doi.org/10.2514/6.2000-4877
https://doi.org/10.2514/6.2000-4877
Publikováno v:
41st Structures, Structural Dynamics, and Materials Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5c6886380ee824ff7f3d58852036fc5f
https://doi.org/10.2514/6.2000-1664
https://doi.org/10.2514/6.2000-1664