Abstract
The experimental study has been carried out to investigate the self-excited shock wave oscillation in a transonic wind tunnel using a circular arc airfoil (chord length of 120 mm, thickness of 15%). Shock wave position of each side and wake position were simultaneously measured by using two line scan cameras (line scan frequency of 32 kHz). Shock wave and wake fluctuations are analyzed by the wavelet transform with Gabor wavelet. The results show that the phase difference between shock wave fluctuations of each side are almost 180 degrees, and the phase difference between shock wave and wake fluctuations was fixed in spite of the change of the frequency.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callMore From: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
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.
