dc.contributor.author |
Kounadis, AN |
en |
dc.date.accessioned |
2014-03-01T01:06:24Z |
|
dc.date.available |
2014-03-01T01:06:24Z |
|
dc.date.issued |
1985 |
en |
dc.identifier.issn |
0001-1452 |
en |
dc.identifier.uri |
https://dspace.lib.ntua.gr/xmlui/handle/123456789/9352 |
|
dc.relation.uri |
http://www.scopus.com/inward/record.url?eid=2-s2.0-0022242923&partnerID=40&md5=8ea2b5fc767dcb0dbbcdae067efef401 |
en |
dc.subject.classification |
Engineering, Aerospace |
en |
dc.subject.other |
VIBRATIONS - Analysis |
en |
dc.subject.other |
FRAMED STRUCTURE VIBRATIONS |
en |
dc.subject.other |
SLENDER BAR VIBRATION |
en |
dc.subject.other |
BARS |
en |
dc.title |
BENDING EIGENFREQUENCIES OF A TWO-BAR FRAME INCLUDING THE EFFECT OF AXIAL INERTIA. |
en |
heal.type |
journalArticle |
en |
heal.language |
English |
en |
heal.publicationDate |
1985 |
en |
heal.abstract |
It has been found that the effect of axial inertia on the lateral vibrations of a two-bar frame can decrease its fundamental eigenfrequency considerably if the mass of the joint is taken into account. If the aforementioned joint mass is neglected, this effect diminishes the bending eigenfrequencies; however, it might be appreciable only for frames in which a high length ratio is combined with a low moment of inertia and low slenderness ratios. |
en |
heal.publisher |
AMER INST AERONAUT ASTRONAUT |
en |
heal.journalName |
AIAA journal |
en |
dc.identifier.isi |
ISI:A1985AUX0500032 |
en |
dc.identifier.volume |
23 |
en |
dc.identifier.issue |
12 |
en |
dc.identifier.spage |
2000 |
en |
dc.identifier.epage |
2002 |
en |