Experimental Investigation on Aerodynamic Characteristics of Propeller in a Ducted-Fan Type VTOL UAV

Article Preview

Abstract:

An experimental investigation was completed with the objective of determining the performance characteristics of propeller in a Ducted-Fan Type VTOL UAV. The model consisted of three groups of two-bladed propellers with or withou an annular duct. The propellers share the same diameter but differernt blade pitchs.Model variations included the changes of the propeller and the duct shrouded combination. Static propulsion test data showed figure of lift increases with increasing blade pitch. The coaxial propellers lift did not perform as 2 times of the single propeller lift.The duct increase the duct fan system lift effectively.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

12-15

Citation:

Online since:

December 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2015 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Ko A, Ohanian O J, Gelhausen P. Ducted fan UAV modeling and simulation in preliminary design, 2007[C].

DOI: 10.2514/6.2007-6375

Google Scholar

[2] Choi Y, Suk J, Hong S. Static Analysis of a Small Scale Ducted-Fan UAV using Wind Tunnel Data[J]. International Journal of Aeronautical and Space Sciences, 2012, 13: 34-42.

DOI: 10.5139/ijass.2012.13.1.34

Google Scholar

[3] Ohanian O J, Karni E D, Londenberg W K, et al. Ducted-fan force and moment control via steady and synthetic jets[J]. Journal of Aircraft, 2011, 48(2): 514-526.

DOI: 10.2514/1.c031110

Google Scholar

[4] Shuai W, Xiao-hui Q. Aerodynamic data model analysis and simulation of ducted fan UAV, 2011[C].

DOI: 10.1109/icecc.2011.6066382

Google Scholar

[5] Karachun K. Analysis of Ducted Fan Flows Using an Immersed Boundary Method[D]. Pennsylvania State University, (2008).

Google Scholar

[6] Ning-jun F, Jia X, Ji-wei Y. Numerical study on aerodynamic characteristics of ducted fan aircraft[J]. Journal of Beijing institute of technology, 2010, 19(1).

Google Scholar