Selection Of Airfoil For LSU-05 Aircraft Wing With Numerical Aerodynamic Analysis

Dana Hediana and Sinung Tirtha Pinindriya and Ardanto M.Pramutadi (2013) Selection Of Airfoil For LSU-05 Aircraft Wing With Numerical Aerodynamic Analysis. Proceedings SIPTEKGAN XVII-2013. pp. 1-6. ISSN 978-979-1458-74-0

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Abstract

Analysis with numerical method has been done for the selection of LSU-05 unmanned vehicle airfoil.The analysis process is done by comparing four airfoil’s performance at a certain reynolds number. The four airfoil shapes are compared by comparing the simulation result of their aerodynamical properties such as lift coefficient, drag coefficient, and the polar drag. The needs of the aircraft itself is to be able to carry a payload of 30 kg, range of 200 km, and endurance of 3 hours. The NACA 4415 airfoil is chosen because it meets the requirement for LSU-05.

Item Type: Article
Uncontrolled Keywords: airfoil, LSU-05, aerodynamics, subsonic speed.
Subjects: Teknologi Penerbangan dan Antariksa > Penelitian, Pengembangan, Perekayasaan, dan Pemanfaatan > Teknologi Aeronautika
Divisions: Deputi Teknologi Penerbangan Dan Antariksa > Pusat Teknologi Penerbangan
Depositing User: Een Rohaeni
Date Deposited: 23 Mar 2021 01:48
Last Modified: 24 Mar 2021 08:15
URI: http://repositori.lapan.go.id/id/eprint/488

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