Publication detail

Experimental modal analysis of plane wing

HOUFEK, L. ČECHÁK, T. KREJČÍ, P.

Original Title

Experimental modal analysis of plane wing

Type

conference paper

Language

English

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

Modal analysis, plane wing

Authors

HOUFEK, L.; ČECHÁK, T.; KREJČÍ, P.

RIV year

2007

Released

24. 4. 2007

Publisher

Spectris Praha spol. s r.o.

Location

Praha

ISBN

978-80-239-9240-3

Book

5. setkání uživatelů PULSE

Pages from

30

Pages to

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"
}