Abstract
An experimental study of wall pressure fluctuations beneath a turbulent boundary layer was carried out on a plate model with a streamwise varying pressure gradient along the plate length. The wall pressure fluctuations were measured with flush-mounted Kulite sensors, and mean velocity measurements across the boundary layer were performed by using a single-wire hot-wire anemometer. A variety of streamwise pressure distributions were imposed by changing the position and the angle of attack of a NACA 0012 airfoil installed above the plate. The effect of the upstream flow history on the wall pressure spectra in the presence of the streamwise varying pressure gradient was studied. Spectral attenuation due to the spatial averaging associated with a finite sensor size was corrected via the Corcos correction. The results show that the Corcos correction to the measured Kulite spectra leads to an overprediction of the spectral intensity at medium frequencies and an underprediction at high frequencies. Hence, a new correction is proposed based on the measured spectral attenuation. Finally, the measurements also indicate that even slight imperfections in sensor mounting and relatively weak upstream flow disturbances can have a significant influence on the measured spectra of the wall pressure fluctuations.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
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.