General aviation aircraft generally uses the piston engines and propellers as its power plant. The performance calculation of the propeller is of great significance in the phase of the plane design. Based on the standard strip analysis, this paper presents a numerical procedure, and carries on the calculation and analysis of a certain type of propeller performance. It includes, thrust coefficient changes with the advance ratio; torque coefficient changes with the advance ratio; power coefficient changes with the advance ratio; propeller efficiency changes with the advance ratio. Compared with the results of the tunnel test, the paper verifies the rationality of the calculation results.
LIU Yuan-qiang, GUO Jin-suo, XIANG Song, TONG Sheng-xi, JIANG Wen-hui
. Aerodynamic performances calculation of propellers based on standard strip analysis[J]. Journal of Shenyang Aerospace University, 2013
, 30(1)
: 43
-46
.
DOI: 10.3969/j.issn.2095-1248.2013.01.010
[1]Quentin R.wald.The aerodynamics of propellers[J].Progress in Aerospace Sciences, 2006, 42:85-128.
[2]S.D’Angelo, F.Berardi, E.Minisci.Aerodyn-amics of propellers with parametric conside-ration on the optimal design[R]Department of Aeronautical and Space Engineering Politecnico di Torino, Turin-Italy, 2007.
[3]刘沛清.空气螺旋桨理论及其应用[M].北京:北京航空航天大学出版社, 2006.
[4]钱翼稷.空气动力学[M].北京:北京航空航天大学出版社, 2006.
[5]李周复.风洞特种试验技术[M].北京:航空工业出版社, 2010.
[6]陈杰.MATLAB宝典(第3版)[M].北京:电子工业出版社, 2011.
[7]Simonetti, F., Ardito Marretta, R.M., “A numerical variational approach forrotor pro-peller aerodynamics in axial flight”[J].Computer Modeling in Engineering & Sciences, 2000(1):3.
[8]Heine B, Mack S, Kurz A, et al.Aerodynamic scaling of general aviation airfoil for low reynolds number application[C].The 38th Fluid Dynamics Conference and Exhibit.Seattle, Washington:AIAA, 2008.
[9]Liu Qing, Li Jie, Zhou Zhou.Low reynolds number high-lift airfoil design for HALE concept UAV[C].The 24th AIAA Applied Aerodynamics Conference.San Francisco, California:AIAA, 2006.
[10]Colozza A, Corportaion A.Overview of innovative aircraft power and propulsion systems and their applications for planetary explorationTM-2003-212459[R].Washington:NASA, 2003.
[11]Moffitt B A, Bradley T H, Parekh D E, et al.Validation of vortex propeller theory for UAV design with uncertainty analysis[C].The 46th AIAA Aerospace Sciences Meeting and Exhibit.Reno, Nevada:AIAA, 2008.
[12]Hallissy J M, Chattot J J.Validation of a helicoidal vortex model with NREL unsteady aerodynamic experiment[C].The 43th AIAA Aerospace Sciences Meeting and Exhibit.Reno, Nevada:AIAA, 2005.
[13]Wald QR.The Wright Brothers propeller theory and design.AIAA Paper 2001-3386, Joint Propulsion Conference, SaltLakeCity, 2001.
