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PEŠÁK, M. KATRŇÁK, T.
Originální název
OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING-EXPERIMENTAL VERIFICATION
Typ
článek ve sborníku ve WoS nebo Scopus
Jazyk
angličtina
Originální abstrakt
The main goal in modern aircraft structural design is decreasing the weight of airplane construction. The weight along with reliability of the construction is the basic parameter which shows success or non-success of the airplane. The option how to decrease the weight of the airplane construction is to use a stiffened panel. The stiffened panel is the part of the construction which is composed of longitudinal reinforcing member(stringer) and skin. The optimal position of these stringers and their dimensions will be the main goal of this paper.
Klíčová slova
stiffened panel, buckling, structural optimization, airplane structure
Autoři
PEŠÁK, M.; KATRŇÁK, T.
Rok RIV
2007
Vydáno
6. 7. 2007
Nakladatel
Západočeská univerzita v Plzni
Místo
Plzeň
ISBN
978-80-7043-597-7
Kniha
Proceedings-5th International PhD Conference on Mechanical Engineering PhD 2007
Edice
Číslo edice
5
Strany od
189
Strany do
192
Strany počet
4
BibTex
@inproceedings{BUT28146, author="Miroslav {Pešák} and Tomáš {Katrňák}", title="OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING-EXPERIMENTAL VERIFICATION", booktitle="Proceedings-5th International PhD Conference on Mechanical Engineering PhD 2007", year="2007", series="2007", number="5", pages="189--192", publisher="Západočeská univerzita v Plzni", address="Plzeň", isbn="978-80-7043-597-7" }