Author:
Staśko Tomasz,Majkut Mirosław,Dykas Sławomir,Smołka Krystian
Abstract
A fan with cycloidal rotor (CRF) becomes a popular idea in wide application such as aviation, HVAC (heat, ventilation and air conditioning) or marine propeller systems. This is due to advantages such as direct control of the flow direction, larger flow rates than in a conventional machines without cycloidal control. In the presented article, velocity fields of CRF placed in a rectangular channel was measured, using Laser Doppler Anemomentry (LDA) method and thermoanemometric probe (TA).
Reference15 articles.
1. Benedict M., Fundamental understanding of cycloidal - rotor concept for micro air vehicle applications. (2010).
2. Augusto J., Monteiro L., Pâscoa J., Xisto C., Aerodynamic optimization of cyclorotors. Aircraft Engineering and Aerospace Technology. (2016).
3. Geometrical Parameters Influencing the Aerodynamic Efficiency of a Small-Scale Self-Pitch High-Solidity VAWT
4. Xisto C., Leger J., Pâscoa J., Gagnon L., Masarati P., Angeli D., Dumas A., Parametric Analysis of a Large - scale Cycloidal Rotor in Hovering Conditions, July (2016), Journal of Aerospace Engineering 30(1).
5. Andrisani A., Angeli D., Dumas A., Optimal pitching schedules for a cycloidal rotor in hovering August (2016), Aircraft Engineering and Aerospace Technology 88(5)
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献