CD Skripsi

Analisis Aerodinamika Pada Pesawat Tanpa Awak Serindit V-2 Menggunakan Metode Komputasional Dinamika Fluida

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ABSTRACT
Serindit V-2 is an unmanned aircraft by the Serindit Aero UAV research
team. It has the ability to fly rapidly in order to compete in KRTI in the Racing
Plane division. Although it has been successfully produced and able to fly,
comprehensive research on aerodynamic of Serindit V-2 aircraft flying behavior
has never been done before. Aerodynamic research need to be conducted to improve
the aircraft performance such as flying capability, air resistance efficiency and etc.
This study aims to determine the value of flow characteristic such as coefficient of
drag, lift, moment and pressure distribution based on fluid flow that occurs in the
aircraft with variations of Angle of Attack and air velocity. The method used is
CFD (Computational Fluid Dynamic) which is a computer-based numerical method
and performed with an iterative procedure to predict aerodynamic characteristics
and fluid flow phenomena on the aircraft surface. Simulations were carried out
using Ansys Fluent 2017 software on the Serindit V-2 aircraft model sourced from
the Serindit Aero Team. The result of the lift coefficient value is CLo = 0.3666 and
CLMax value = 1.42626 at α 13o. The CDo obtained was 0.0589258. While the CMo
value obtained is -8.34 x 10-5.
Keyword: Flow Characteristics, CFD, Ansys Fluent

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Ketersediaan

Informasi Detail

Judul Seri

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No. Panggil

07 03. 121 (0021)

Penerbit

Pekanbaru : Universitas Riau – Fakultas Teknik – Teknik Mesin., 2021

Deskripsi Fisik

ix, 232 hlm.; ill.: 29 cm

Bahasa

Indonesia

ISBN/ISSN

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Klasifikasi

07 03. 121 (0021)

Tipe Isi

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Tipe Media

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Tipe Pembawa

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Edisi

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Subjek

TEKNIK MESIN

Info Detail Spesifik

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Pernyataan Tanggungjawab

Daus

Versi lain/terkait

Lampiran Berkas

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