Optimization of Trailing-Edge Serrations to Reduce Open-Rotor Tonal Interaction Noise

Author:

Jaron Robert1,Moreau Antoine2,Guérin Sébastien3,Schnell Rainer4

Affiliation:

1. Institute of Propulsion Technology, German Aerospace Center (DLR), Müller-Breslau-Straße 8, Berlin 10623, Germany e-mail:

2. Institute of Propulsion Technology German Aerospace Center (DLR), Müller-Breslau-Straße 8, Berlin 10623, Germany

3. Institute of Propulsion Technology, German Aerospace Center (DLR), Müller-Breslau-Straße 8, Berlin 10623, Germany

4. Institute of Propulsion Technology, German Aerospace Center (DLR), Linder Höhe, Cologne 51147, Germany

Abstract

A major source of contra-rotating open rotor (CROR) tonal noise is caused by the interaction of the front-rotor (FR) wakes with the aft-rotor blades. Inspired by chevron nozzles, which increase the mixing process in jet shear layers, serrations are implemented at the FR trailing-edge in order to increase the wake mixing and thus reduce the tones. The depth and width of the serrations are optimized with a multi-objective, metamodel-assisted evolutionary algorithm. For each member, a steady-state Reynolds-averaged Navier–Stokes (RANS) simulation is performed, which is coupled with an analytical noise prediction method in order to evaluate the noise reduction due to the serrations. The results confirm that tonal interaction noise can be reduced by means of trailing-edge serrations. It is found that the major noise reduction mechanism for wake interaction is attributed to increased destructive interferences occurring in spanwise direction. The tonal noise generated through the interaction of the rear rotor (RR) potential field with the FR trailing edge is also slightly reduced because of the circumferential and axial shift of the serrated trailing edge. Furthermore, the present study demonstrates the feasibility of performing an acoustic optimization with a hybrid approach that predicts the noise analytically and extracts the aerodynamic input data from a steady-state RANS flow solution.

Publisher

ASME International

Subject

Mechanical Engineering

Reference31 articles.

1. Performance Prediction and Progress Towards Multi-Disciplinary Design of Contra-Rotating Open Rotors;Aeronaut. J.,2014

2. How to Improve Open Rotor Aerodynamics at Cruise and Take-Off;Aeronaut. J.,2014

3. The Effect of Front-to-Rear Propeller Spacing on the Interaction Noise at Cruise Conditions of a Model Counterrotation Propeller Having a Reduced Diameter aft Propeller,1988

4. Noise of a Model Counterrotation Propeller With Reduced AFT Rotor Diameter at Simulated Takeoff/Approach Conditions (F7/A3),1988

5. Analytical Prediction of Wake-Interaction Noise in Counter-Rotation Open Rotors,2011

Cited by 25 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

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3