A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variation

A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variation

NACA0012H is an airfoil type that could be used for Unmanned Aerial Vehicle Medium Altitude Long Endurance. This experiment was used to analyze stress in the surface of Tail of UAV MALE that was caused by air flow. The experiment was conducted using Computational Fluid Dynamics Software. Two designs...

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Main Authors: Riza Rahmat, Kurniawan Dicky, Wicaksono Arif Budi
Format: Article
Language:English
Published: EDP Sciences 2018-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201815401115
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spelling doaj-135e1f6f78d34658a0d565eba389a4df2021-02-02T03:31:59ZengEDP SciencesMATEC Web of Conferences2261-236X2018-01-011540111510.1051/matecconf/201815401115matecconf_icet4sd2018_01115A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variationRiza RahmatKurniawan DickyWicaksono Arif BudiNACA0012H is an airfoil type that could be used for Unmanned Aerial Vehicle Medium Altitude Long Endurance. This experiment was used to analyze stress in the surface of Tail of UAV MALE that was caused by air flow. The experiment was conducted using Computational Fluid Dynamics Software. Two designs of tail, horizontal and V-tail, were considered to simulate pressure occurred on the surface of leading edge, chamber and trailing edge. The simulation was developed varying the speed of the UAV MALE. The results showed that pressure occurred on the surface of horizontal tail higher than pressure on the V-tail.https://doi.org/10.1051/matecconf/201815401115
collection DOAJ
language English
format Article
sources DOAJ
author Riza Rahmat
Kurniawan Dicky
Wicaksono Arif Budi
spellingShingle Riza Rahmat
Kurniawan Dicky
Wicaksono Arif Budi
A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variation
MATEC Web of Conferences
author_facet Riza Rahmat
Kurniawan Dicky
Wicaksono Arif Budi
author_sort Riza Rahmat
title A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variation
title_short A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variation
title_full A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variation
title_fullStr A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variation
title_full_unstemmed A comparative pressure analysis of air flow between horizontal and V-Tail of UAV MALE of NACA0012H with speed variation
title_sort comparative pressure analysis of air flow between horizontal and v-tail of uav male of naca0012h with speed variation
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2018-01-01
description NACA0012H is an airfoil type that could be used for Unmanned Aerial Vehicle Medium Altitude Long Endurance. This experiment was used to analyze stress in the surface of Tail of UAV MALE that was caused by air flow. The experiment was conducted using Computational Fluid Dynamics Software. Two designs of tail, horizontal and V-tail, were considered to simulate pressure occurred on the surface of leading edge, chamber and trailing edge. The simulation was developed varying the speed of the UAV MALE. The results showed that pressure occurred on the surface of horizontal tail higher than pressure on the V-tail.
url https://doi.org/10.1051/matecconf/201815401115
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