Change search
ReferencesLink to record
Permanent link

Direct link
Upper-bound flutter speed estimation using the mu-k method
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Flight Dynamics.
2005 (English)In: Journal of Aircraft, ISSN 0021-8669, E-ISSN 1533-3868, Vol. 42, no 2, 555-557 p.Article in journal (Refereed) Published
Abstract [en]

The use of upper-bound μ-k estimation method in the development of robust flutter analysis and flutter testing, was described. Since only the frequency-domain aerodynamic forces are required to compute μ(k), established aerodynamic methods can be used for the robust flutter analysis. A robust flutter analysis considering wing-tip aerodynamic uncertainty was developed in MATLAB® for a wind-tunnel model in low-speed airflow. The results show that the extended procedure for robust flutter analysis was successfully applied to a wind-tunnel model in low-speed airflow.

Place, publisher, year, edition, pages
2005. Vol. 42, no 2, 555-557 p.
Keyword [en]
Air density, Flutter equations, Flutter speed, Mach number
National Category
Aerospace Engineering
URN: urn:nbn:se:kth:diva-14662ISI: 000228284100032ScopusID: 2-s2.0-18144416970OAI: diva2:332703

QC 20100525

Available from: 2010-08-05 Created: 2010-08-05 Last updated: 2014-12-02Bibliographically approved

Open Access in DiVA

No full text


Search in DiVA

By author/editor
Borglund, Dan
By organisation
Flight Dynamics
In the same journal
Journal of Aircraft
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 51 hits
ReferencesLink to record
Permanent link

Direct link