publication . Article . 2018

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

Riza Rahmat; Kurniawan Dicky; Wicaksono Arif Budi;
Open Access
  • Published: 01 Jan 2018 Journal: MATEC Web of Conferences, volume 154, page 1,115 (eissn: 2261-236X, Copyright policy)
  • Publisher: EDP Sciences
Abstract
<jats:p>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 <jats:italic>V</jats:italic>-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 <jats:italic>V</jats:italic>-...
Subjects
free text keywords: Leading edge, Computational fluid dynamics, business.industry, business, Altitude, Trailing edge, Pressure analysis, Mechanics, V-tail, Airfoil, Airflow, Engineering (General). Civil engineering (General), TA1-2040
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1. Babu, P. Hussain, Rodriguez Arthurs S.A, S. Mahaboob Basha, Sadiq. P., Design and Analysis of V-Tail Unmanned Air Vehicle (UAV) for Surveillance Application, International Journal of Engineering Trends and Technology (IJETT), 32, Number 3 (2016)

2. Azeez VP, Abdul, John Paul CFD Analysis of NACA 63-018 Airfoil at Different Reynolds-Number, International Journal of Engineering Trends and Technology (IJETT), 12, No. 5 (2014)

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publication . Article . 2018

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

Riza Rahmat; Kurniawan Dicky; Wicaksono Arif Budi;