Abstract
The aerodynamic behavior of two self-oscillating sections are predicted by nonlinear k− ε model. One is the parallel rectangular cross-section ( B/ D=15; 2 d= B′; B: total width; D: height; B′: single width; 2 d: space of the sections) and another is the flat box girder cross-section. The section has the special feature that the box girder is separated and the vertical and the horizontal stabilizers are installed. At first, in order to investigate the applicability of the numerical method, the calculated results of aerodynamic behavior were compared with the experimental data for the parallel rectangular cross-section such as the priority test. Secondly, the method was applied to the flat box girder cross-section, and the aerodynamic instability mechanism on the stabilizer was examined from the calculated results of the flow pattern and the unsteady pressure characteristics.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
More From: Journal of Wind Engineering and Industrial Aerodynamics
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.