A METHOD FOR PREDICTING CONTRA ROTATING PROPELLERS OFF-DESIGN PERFORMANCE

被引:0
|
作者
Dubosc, Matthieu [1 ]
Tantot, Nicolas [1 ]
Beaumier, Philippe [2 ]
Delattre, Gregory [2 ]
机构
[1] Snecma Safran Grp, Preliminary Design Dept, F-77550 Moissy Cramayel, France
[2] Onera French Aerosp Lab, F-92190 Meudon, France
来源
PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 1A | 2014年
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中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article presents a method for predicting contra rotating propellers individual and total performance which is fast and robust enough to be used in performance engine cycle and engine subsystems detailed design. The method is based on the use of single propeller maps and models mutual induced velocities thanks to one-dimensional theories. These velocities are responsible for interferences between propellers. This article goes through the assumptions on which stands the proposed method and shows that it is relevant compared against more complex methods such as lifting line theory and definitively provides a valuable easy-to-enforce preliminary design tool for open rotor propulsor controls sizing.
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页数:10
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