Numerical Simulation of the Static and Dynamic Aerodynamics of a UAV under Wake Flows

Frequent flight conflicts will be observed as the number of aircrafts increases, and such conflicts will cause unprecedented challenges in flight safety; thus, the flight characteristics of small aircrafts under the wake flow of a large airliner should be thoroughly analyzed. Combined with the slidi...

Full description

Saved in:
Bibliographic Details
Main Authors: Bai-gang Mi, Hao Zhan
Format: Article
Language:English
Published: Wiley 2019-01-01
Series:Journal of Advanced Transportation
Online Access:http://dx.doi.org/10.1155/2019/6326794
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1832559208395964416
author Bai-gang Mi
Hao Zhan
author_facet Bai-gang Mi
Hao Zhan
author_sort Bai-gang Mi
collection DOAJ
description Frequent flight conflicts will be observed as the number of aircrafts increases, and such conflicts will cause unprecedented challenges in flight safety; thus, the flight characteristics of small aircrafts under the wake flow of a large airliner should be thoroughly analyzed. Combined with the sliding mesh technique, a computational fluid dynamics (CFD) method is proposed in this paper to simulate three wake flow patterns, i.e., wingtip vortex, jet flow, and propeller slipstream, and then, the static and dynamic derivatives that represent the stability of the fly wing under the wake flow are identified by using the least squares method. The results demonstrate that both the steady and unsteady aerodynamics of the fly wing are affected by wake flows: wingtip vortices increase the lift-to-drag ratio and considerably change the dynamic damping; jet flow reduces both the static and dynamic damping; and propeller slipstream leads to slow variations in the dynamic damping and decreases in the lift-to-drag ratio.
format Article
id doaj-art-53d41316eb80431fbec388db20fd5c55
institution Kabale University
issn 0197-6729
2042-3195
language English
publishDate 2019-01-01
publisher Wiley
record_format Article
series Journal of Advanced Transportation
spelling doaj-art-53d41316eb80431fbec388db20fd5c552025-02-03T01:30:37ZengWileyJournal of Advanced Transportation0197-67292042-31952019-01-01201910.1155/2019/63267946326794Numerical Simulation of the Static and Dynamic Aerodynamics of a UAV under Wake FlowsBai-gang Mi0Hao Zhan1School of Aerospace Engineering, Tsinghua University, Beijing 100084, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an, Shaanxi 710072, ChinaFrequent flight conflicts will be observed as the number of aircrafts increases, and such conflicts will cause unprecedented challenges in flight safety; thus, the flight characteristics of small aircrafts under the wake flow of a large airliner should be thoroughly analyzed. Combined with the sliding mesh technique, a computational fluid dynamics (CFD) method is proposed in this paper to simulate three wake flow patterns, i.e., wingtip vortex, jet flow, and propeller slipstream, and then, the static and dynamic derivatives that represent the stability of the fly wing under the wake flow are identified by using the least squares method. The results demonstrate that both the steady and unsteady aerodynamics of the fly wing are affected by wake flows: wingtip vortices increase the lift-to-drag ratio and considerably change the dynamic damping; jet flow reduces both the static and dynamic damping; and propeller slipstream leads to slow variations in the dynamic damping and decreases in the lift-to-drag ratio.http://dx.doi.org/10.1155/2019/6326794
spellingShingle Bai-gang Mi
Hao Zhan
Numerical Simulation of the Static and Dynamic Aerodynamics of a UAV under Wake Flows
Journal of Advanced Transportation
title Numerical Simulation of the Static and Dynamic Aerodynamics of a UAV under Wake Flows
title_full Numerical Simulation of the Static and Dynamic Aerodynamics of a UAV under Wake Flows
title_fullStr Numerical Simulation of the Static and Dynamic Aerodynamics of a UAV under Wake Flows
title_full_unstemmed Numerical Simulation of the Static and Dynamic Aerodynamics of a UAV under Wake Flows
title_short Numerical Simulation of the Static and Dynamic Aerodynamics of a UAV under Wake Flows
title_sort numerical simulation of the static and dynamic aerodynamics of a uav under wake flows
url http://dx.doi.org/10.1155/2019/6326794
work_keys_str_mv AT baigangmi numericalsimulationofthestaticanddynamicaerodynamicsofauavunderwakeflows
AT haozhan numericalsimulationofthestaticanddynamicaerodynamicsofauavunderwakeflows