Zobrazeno 1 - 10
of 27
pro vyhledávání: '"John Rajadas"'
Publikováno v:
2007 Annual Conference & Exposition Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea2de2c4c30352f54eaa5493bf1d9c2c
https://doi.org/10.18260/1-2--2335
https://doi.org/10.18260/1-2--2335
Autor:
John Rajadas, Bradley Rogers
Publikováno v:
2007 Annual Conference & Exposition Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c348f826f8cd7bede48603c0717b270b
https://doi.org/10.18260/1-2--2150
https://doi.org/10.18260/1-2--2150
Publikováno v:
AIAA Journal. 50:769-777
This paper presents a passive sensing technique for real-time structural health monitoring. In the proposed technique, two reference or healthy state dynamic models are estimated using a nonlinear statistical pattern recognition technique known as th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29370e9ab3902747827040cb788e47e7
https://doi.org/10.2514/1.j050820
https://doi.org/10.2514/1.j050820
Publikováno v:
AIAA Journal. 43:560-571
Ar educed-order model (ROM) for solving an aeroelasticity problem including structural and aerodynamic nonlinearities is introduced. The aerodynamic system is identified using a Volterra-based ROM. The appropriate procedures needed for the identifica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::694b2917aab7268951f45e5da8b6d32c
https://doi.org/10.2514/1.10971
https://doi.org/10.2514/1.10971
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:
Engineering Optimization. 33:113-133
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::15e96dc79a2315813cef8141c9e21ca8
https://doi.org/10.1080/03052150008940913
https://doi.org/10.1080/03052150008940913
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
Publikováno v:
Engineering Optimization. 31:25-51
A multidisciplinary design optimization procedure is developed for the simultaneous improvement of sonic boom, aerodynamic and structural performance of high speed aircraft. The coupled problem is decomposed into two levels of optimization. At the fi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::357e623a0f1296dd7207352a0184edab
https://doi.org/10.1080/03052159808941364
https://doi.org/10.1080/03052159808941364
Publikováno v:
Journal of Aircraft. 33:1123-1130
A design optimization procedure for improved sonic boom and aerodynamic performance of highspeed aircraft has been developed. The multiobjective optimization procedure simultaneously minimizes the primary sonic boom and the drag-to-lift ratio of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b5fdca43d9b03ada463e6158fc902eae
https://doi.org/10.2514/3.47066
https://doi.org/10.2514/3.47066