Presenter(s)
Muhammad Omar Memon, Kevin Wabick
Files
Download Project (1.2 MB)
Description
The lens of exergy is used to investigate a wingtip vortex in the near wake over a range of angles of attack. Exergy is the measure of thermodynamically “available” energy as determined through the more discriminating second law of thermodynamics. Experiments were conducted in a water tunnel at ILR Aachen. The data was taken three chord lengths downstream in the Trefftz plane of an aspect ratio (AR) 5 Clark-Y wing with a square edged wingtip using Particle Image Velocimetry (PIV). Intuitively, the minimum available energy state is expected to correspond to the maximum lift to drag ratio angle of attack. This, however, is not the case here. Most interestingly, although only 2-d Trefftz plane data was used to obtain the exergy distribution across the individual wingtip vortices, the crossover point for the out of plane change from wake-like to jet-like wingtip vortex core axial flow (indicating the peak lift to drag ratio) is identified by the in-plane exergy distribution. This crossover point is not identifiable in the evaluation of any other characteristics calculated from in-plane quantities. Consequently, the exergy method holds promise as a metric for the improvement of aircraft performance through the reduction of lift induced drag.
Publication Date
4-9-2014
Project Designation
Graduate Research
Primary Advisor
Aaron Altman
Primary Advisor's Department
Mechanical and Aerospace Engineering
Keywords
Stander Symposium project
Disciplines
Arts and Humanities | Business | Education | Engineering | Life Sciences | Medicine and Health Sciences | Physical Sciences and Mathematics | Social and Behavioral Sciences
Recommended Citation
"Wingtip Vortices from an Exergy Based Perspective" (2014). Stander Symposium Projects. 528.
https://ecommons.udayton.edu/stander_posters/528
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