Wake-Tailplane Interaction of a Slingsby Firefly Aircraft

Author:

Lawson Nicholas J.ORCID,Davies Simon G.,Khanal BidurORCID,Hoff Rein I.

Abstract

This paper presents in-flight measurements of the interaction of the wing wake of a stalled Slingsby T67 Firefly light aircraft with the aircraft tailplane. Tailplane data was recorded by a GoPro360 camera and analyzed using spatial correlation methods. The tailplane movement and corresponding spectra indicate that the aerodynamic wake shedding frequency closely matches the resonant frequency of the tailplane, resulting in a significant excitation of the structure during heavy stall. Large magnitude, lower frequency tailplane movement was also identified by analysis of the pitch attitude from the image data, with results consistent in post-stall behavior reported by previous modelling and measurements.

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference13 articles.

1. Wake vortex characteristics of transport aircraft;Breitsamter;Prog. Aerosp. Sci.,2011

2. Wind turbine wake aerodynamics;Vermeer;Prog. Aerosp. Sci.,2003

3. Vibrations of simplified rudder induced by propeller wake;Zhang;Phys. Fluids,2021

4. Vortex-Body interactions;Rockwell;Ann. Rev. Fluid Mech.,1998

5. Deflected wake interaction of tandem flapping foils;Lagopoulos;J. Fluid Mech.,2020

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