Experimental results of a fluttering profile in the wind tunnel
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F12%3A00378677" target="_blank" >RIV/61388998:_____/12:00378677 - isvavai.cz</a>
Result on the web
—
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
Experimental results of a fluttering profile in the wind tunnel
Original language description
The two-dimensional flow patterns around the profile NACA 0015vibrating in self-excitation modes were measured in the wind tunnel by optical methods. The profile with two-degree-of freedom moved in the vertical direction and rotated around the elastic axis in 1/3 of the profile chord. The Mach numbers for the self-excited vibrations were in the interval 0.2 ? 0.45. Results of the interferometric measurement and the profile kinematic movements during the self-oscillations are presented.
Czech name
—
Czech description
—
Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
—
Result continuities
Project
<a href="/en/project/GA101%2F09%2F1522" target="_blank" >GA101/09/1522: Experimental investigation of unsteady flow patterns around vibrating airfoil with application in aeroelasticity</a><br>
Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Flow-Induced Vibration
ISBN
978-0-9548583-4-6
ISSN
—
e-ISSN
—
Number of pages
4
Pages from-to
677-680
Publisher name
School of Engineering Trinity College, Dublin
Place of publication
Dublin
Event location
Dublin
Event date
Jul 3, 2012
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
—