Abstract
The authors wish to make the following corrections to their paper [...]
Highlights
In addition to the noise reduction, Talboys and Brücker [14] reported, in their study, on the shear layer stabilization effect that is caused by the trailing flaps on the suction side of the airfoil
This effect could lead to enhanced airfoil performance”
Publisher’s Note: MDPI stays neutral with regard to jurisdictional claims in published maps and institutional affiliations
Summary
Publisher’s Note: MDPI stays neutral with regard to jurisdictional claims in published maps and institutional affiliations. The authors wish to make the following corrections to their paper [1]: In the introduction on page 2 and 3, we would like to add information from two additional literature sources [2,3], the reference number will be updated .
Sign-in/Register to view highlights & summary 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 callDisclaimer: 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.
