Details
| Original language | English |
|---|---|
| Title of host publication | 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014 |
| ISBN (electronic) | 3932182804 |
| Publication status | Published - 2014 |
| Event | 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014 - St. Petersburg, Russian Federation Duration: 7 Sept 2014 → 12 Sept 2014 |
Publication series
| Name | 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014 |
|---|
Abstract
The availability of a Vibration Correlation Technique (VCT) for nondestructive determination of buckling loads of cylindrical shells has obvious advantages. Earlier, a semi-empirical VCT approach has been developed and applied successfully for the prediction of the buckling load of closely stiffened aluminum shells. In the present paper, a possibility to support and improve the estimates of this semi-empirical VCT approach by means of the application of analysis tools is proposed. Two semi-analytical models with different levels of complexity will be used for this purpose. In the two approaches employed, both the nonlinear effect of the static state and the nonlinear effect of the geometric imperfections are represented. These two methods form the basis of an extension of the existing semi-empirical Vibration Correlation Technique for shells, to a VCT in which vibration measurements and analysis tools are combined. In this paper, the capability of the analysis tools which can be used to improve the VCT is illustrated.
Keywords
- Buckling, Nondestructive testing, Structures, Vibration
ASJC Scopus subject areas
- Engineering(all)
- Aerospace Engineering
- Engineering(all)
- Control and Systems Engineering
- Engineering(all)
- Electrical and Electronic Engineering
- Materials Science(all)
Cite this
- Standard
- Harvard
- Apa
- Vancouver
- BibTeX
- RIS
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014. 2014. (29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014).
Research output: Chapter in book/report/conference proceeding › Conference contribution › Research › peer review
}
TY - GEN
T1 - The direct prediction of buckling loads of shells under axial compression using VCT - Towards an upgraded approach
AU - Jansen, E. L.
AU - Abramovich, H.
AU - Rolfes, R.
PY - 2014
Y1 - 2014
N2 - The availability of a Vibration Correlation Technique (VCT) for nondestructive determination of buckling loads of cylindrical shells has obvious advantages. Earlier, a semi-empirical VCT approach has been developed and applied successfully for the prediction of the buckling load of closely stiffened aluminum shells. In the present paper, a possibility to support and improve the estimates of this semi-empirical VCT approach by means of the application of analysis tools is proposed. Two semi-analytical models with different levels of complexity will be used for this purpose. In the two approaches employed, both the nonlinear effect of the static state and the nonlinear effect of the geometric imperfections are represented. These two methods form the basis of an extension of the existing semi-empirical Vibration Correlation Technique for shells, to a VCT in which vibration measurements and analysis tools are combined. In this paper, the capability of the analysis tools which can be used to improve the VCT is illustrated.
AB - The availability of a Vibration Correlation Technique (VCT) for nondestructive determination of buckling loads of cylindrical shells has obvious advantages. Earlier, a semi-empirical VCT approach has been developed and applied successfully for the prediction of the buckling load of closely stiffened aluminum shells. In the present paper, a possibility to support and improve the estimates of this semi-empirical VCT approach by means of the application of analysis tools is proposed. Two semi-analytical models with different levels of complexity will be used for this purpose. In the two approaches employed, both the nonlinear effect of the static state and the nonlinear effect of the geometric imperfections are represented. These two methods form the basis of an extension of the existing semi-empirical Vibration Correlation Technique for shells, to a VCT in which vibration measurements and analysis tools are combined. In this paper, the capability of the analysis tools which can be used to improve the VCT is illustrated.
KW - Buckling
KW - Nondestructive testing
KW - Structures
KW - Vibration
UR - http://www.scopus.com/inward/record.url?scp=84910652635&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84910652635
T3 - 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
BT - 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
T2 - 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
Y2 - 7 September 2014 through 12 September 2014
ER -