Effects of SJA boundary conditions on predicting the aerodynamic behavior of NACA 0015 airfoil in separated condition

标题
Effects of SJA boundary conditions on predicting the aerodynamic behavior of NACA 0015 airfoil in separated condition
作者
关键词
Active flow control, Morphing mesh technique, NACA 0015, Oscillatory inlet velocity, Synthetic jet actuators (SJA)
出版物
Journal of Mechanical Science and Technology
Volume 29, Issue 5, Pages 1829-1836
出版商
Springer Nature
发表日期
2015-05-15
DOI
10.1007/s12206-015-0403-8

向作者/读者发起求助以获取更多资源

Reprint

联系作者

Publish scientific posters with Peeref

Peeref publishes scientific posters from all research disciplines. Our Diamond Open Access policy means free access to content and no publication fees for authors.

Learn More

Create your own webinar

Interested in hosting your own webinar? Check the schedule and propose your idea to the Peeref Content Team.

Create Now