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How to improve open rotor aerodynamics at cruise and take-off

Published online by Cambridge University Press:  27 January 2016

C. Hall ,
A. Zachariadis ,
T. Brandvik  and
N. Sohoni
C. Hall*
Affiliation:
University of Cambridge, Whittle Laboratory, Cambridge, UK
A. Zachariadis
Affiliation:
University of Cambridge, Whittle Laboratory, Cambridge, UK
T. Brandvik
Affiliation:
University of Cambridge, Whittle Laboratory, Cambridge, UK
N. Sohoni
Affiliation:
University of Cambridge, Whittle Laboratory, Cambridge, UK
*
[email protected]
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Abstract

A key challenge in open rotor design is getting the optimum aerodynamics at both the cruise and take-off conditions. This is particularly difficult because the operation and the requirements of an open rotor are very different at cruise compared to takeoff. This paper uses CFD results to explore the impact of various design changes on the cruise and take-off flow-fields. The paper then considers how a given open rotor design is best operated at take-off to minimise noise whilst maintaining high thrust. The main findings are that various design modifications can be applied to control the flow features that lead to lost efficiency at cruise and increased noise emission at take-off. A breakdown of the lost power terms from CFD solutions demonstrates how developments in open rotor design have led to reduced aerodynamic losses. At take-off, the operating point of the open rotor should be set such that the non-dimensional lift is as high as possible, without causing significant flow separation. This can be achieved through suitable amounts of re-pitch and speed up applied to a design. Comparisons with fully three-dimensional CFD show that the amount of re-pitch required can be determined using simplified methods such as two-dimensional CFD and a Blade Element Method.

Type
Research Article
Information
The Aeronautical Journal , Volume 118 , Issue 1208 , October 2014 , pp. 1103 - 1123
Copyright
Copyright © Royal Aeronautical Society 2014 

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