Detail publikace
Experimental modal analysis of plane wing
HOUFEK, L. ČECHÁK, T. KREJČÍ, P.
Anglický název
Experimental modal analysis of plane wing
Typ
Stať ve sborníku v databázi WoS či Scopus
Jazyk
en
Originální abstrakt
Experimental modal analysis is used for eigen frequencies and eigen shape of vibration determination. The damping for each eign frequency and interdependency can be also determined by this tool. All these parameters are important for correct design of mechanisms and their reliable operation. The modal analysis of plane wing was performed in range of 6-140Hz. This range was selected because of low sensor sensitivity for low frequencies. The high frequency of this range is good enough for all real exciting frequencies.
Klíčová slova anglicky
Modal analysis, plane wing
Vydáno
2007-04-24
Nakladatel
Spectris Praha spol. s r.o.
Místo
Praha
ISBN
978-80-239-9240-3
Kniha
5. setkání uživatelů PULSE
Strany od–do
30–37
Počet stran
7
BIBTEX
@inproceedings{BUT24068,
author="Lubomír {Houfek} and Tomáš {Čechák} and Petr {Krejčí}",
title="Experimental modal analysis of plane wing",
booktitle="5. setkání uživatelů PULSE",
year="2007",
pages="30--37",
publisher="Spectris Praha spol. s r.o.",
address="Praha",
isbn="978-80-239-9240-3"
}