Detail publikačního výsledku

Experimental modal analysis of plane wing

HOUFEK, L.; ČECHÁK, T.; KREJČÍ, P.

Originální název

Experimental modal analysis of plane wing

Anglický název

Experimental modal analysis of plane wing

Druh

Stať ve sborníku v databázi WoS či Scopus

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.

Anglický 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

Modal analysis, plane wing

Klíčová slova v angličtině

Modal analysis, plane wing

Autoři

HOUFEK, L.; ČECHÁK, T.; KREJČÍ, P.

Vydáno

24.04.2007

Nakladatel

Spectris Praha spol. s r.o.

Místo

Praha

ISBN

978-80-239-9240-3

Kniha

5. setkání uživatelů PULSE

Strany od

30

Strany do

37

Strany počet

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"
}