A novel approach to calculating induced drag from computational fluid dynamics

Early aerodynamic mathematical methods rely on potential flow concepts that formally isolate aerodynamic drag into a profile and an induced drag component. The more recent evolution of Navier–Stokes-based Computational Fluid Dynamics (CFD) methods typically directly computes aerodynamic forces. It d...

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Main Authors: George Loubimov, Michael Kinzel
Format: Article
Language:English
Published: AIP Publishing LLC 2021-07-01
Series:AIP Advances
Online Access:http://dx.doi.org/10.1063/5.0051080
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spelling doaj-d2d589c38df94565a21897f2ba80eaf42021-08-04T13:18:51ZengAIP Publishing LLCAIP Advances2158-32262021-07-01117075009075009-1110.1063/5.0051080A novel approach to calculating induced drag from computational fluid dynamicsGeorge Loubimov0Michael Kinzel1Department of Mechanical and Aerospace Engineering, University of Central Florida, Orlando 32816, Florida, USADepartment of Mechanical and Aerospace Engineering, University of Central Florida, Orlando 32816, Florida, USAEarly aerodynamic mathematical methods rely on potential flow concepts that formally isolate aerodynamic drag into a profile and an induced drag component. The more recent evolution of Navier–Stokes-based Computational Fluid Dynamics (CFD) methods typically directly computes aerodynamic forces. It does so using surface integration of pressure and viscous forces, which does not readily enable conventional separation of profile and induced drag. Isolating induced drag from aerodynamic drag is not well developed using CFD, leading to the present effort that derives a mathematical framework to extract induced drag from CFD model results. The present approach builds on mass, momentum, and energy equation control volume analysis performed within the CFD results. We find that the energy equation provides the necessary means for the closure of quantifying induced drag within the context of minor assumptions. In addition, the results indicate an interesting character in the development of energy losses in the context of induced drag associated with flow reorganization into a tip vortex. The results from the approach indicate accuracy in the method as displayed with good correlation to predictions from analytical and potential flow methods for a variety of wing planforms. Results indicate a novel and efficient method to extract induced drag from CFD models.http://dx.doi.org/10.1063/5.0051080
collection DOAJ
language English
format Article
sources DOAJ
author George Loubimov
Michael Kinzel
spellingShingle George Loubimov
Michael Kinzel
A novel approach to calculating induced drag from computational fluid dynamics
AIP Advances
author_facet George Loubimov
Michael Kinzel
author_sort George Loubimov
title A novel approach to calculating induced drag from computational fluid dynamics
title_short A novel approach to calculating induced drag from computational fluid dynamics
title_full A novel approach to calculating induced drag from computational fluid dynamics
title_fullStr A novel approach to calculating induced drag from computational fluid dynamics
title_full_unstemmed A novel approach to calculating induced drag from computational fluid dynamics
title_sort novel approach to calculating induced drag from computational fluid dynamics
publisher AIP Publishing LLC
series AIP Advances
issn 2158-3226
publishDate 2021-07-01
description Early aerodynamic mathematical methods rely on potential flow concepts that formally isolate aerodynamic drag into a profile and an induced drag component. The more recent evolution of Navier–Stokes-based Computational Fluid Dynamics (CFD) methods typically directly computes aerodynamic forces. It does so using surface integration of pressure and viscous forces, which does not readily enable conventional separation of profile and induced drag. Isolating induced drag from aerodynamic drag is not well developed using CFD, leading to the present effort that derives a mathematical framework to extract induced drag from CFD model results. The present approach builds on mass, momentum, and energy equation control volume analysis performed within the CFD results. We find that the energy equation provides the necessary means for the closure of quantifying induced drag within the context of minor assumptions. In addition, the results indicate an interesting character in the development of energy losses in the context of induced drag associated with flow reorganization into a tip vortex. The results from the approach indicate accuracy in the method as displayed with good correlation to predictions from analytical and potential flow methods for a variety of wing planforms. Results indicate a novel and efficient method to extract induced drag from CFD models.
url http://dx.doi.org/10.1063/5.0051080
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