Publication detail
Experimental modal analysis of plane wing
HOUFEK, L. ČECHÁK, T. KREJČÍ, P.
English title
Experimental modal analysis of plane wing
Type
Paper in proceedings (conference paper)
Language
en
Original abstract
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.
Keywords in English
Modal analysis, plane wing
Released
2007-04-24
Publisher
Spectris Praha spol. s r.o.
Location
Praha
ISBN
978-80-239-9240-3
Book
5. setkání uživatelů PULSE
Pages from–to
30–37
Pages count
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"
}