Simulasi Analisis Kekuatan Struktur Sayap Komposit dengan Finite Element Analysis Menggunakan Material Carbon Fiber, Kevlar, dan Honeycomb

Hangduaril, Charta Wijaya (2024) Simulasi Analisis Kekuatan Struktur Sayap Komposit dengan Finite Element Analysis Menggunakan Material Carbon Fiber, Kevlar, dan Honeycomb. Bachelor thesis, Institut Teeknologi Kalimantan.

	Text 03191038_cover.pdf Download (44kB)
	Text 03191038_statement_of_authenticity.pdf Download (386kB)
	Text 03191038_publishing_agreement.pdf Download (366kB)
	Text 03191038_approval_sheet.pdf Download (132kB)
	Text 03191038_preface.pdf Download (360kB)
	Text 03191038_abstract_id.pdf Download (219kB)
	Text 03191038_abstract_en.pdf Restricted to Repository staff only until 4 May 2026. Download (391kB) | Request a copy
	Text 03191038_table_of_content.pdf Restricted to Repository staff only until 4 May 2026. Download (299kB) | Request a copy
	Text 03191038_illustrations.pdf Restricted to Repository staff only until 4 May 2026. Download (223kB) | Request a copy
	Text 03191038_tables.pdf Restricted to Repository staff only until 4 May 2026. Download (219kB) | Request a copy
	Text 03191038_notations.pdf Restricted to Repository staff only until 4 May 2026. Download (282kB) | Request a copy
	Text 03191038_chapter_1.pdf Restricted to Repository staff only until 4 May 2026. Download (237kB) | Request a copy
	Text 03191038_chapter_2.pdf Restricted to Repository staff only until 4 May 2026. Download (535kB) | Request a copy
	Text 03191038_chapter_3.pdf Restricted to Repository staff only until 4 May 2026. Download (1MB) | Request a copy
	Text 03191038_chapter_4.pdf Restricted to Repository staff only until 4 May 2026. Download (784kB) | Request a copy
	Text 03191038_conclusions.pdf Restricted to Repository staff only until 4 May 2026. Download (224kB) | Request a copy
	Text 03191038_bibliography.pdf Download (249kB)
	Text 03191038_enclosure.pdf Restricted to Repository staff only until 4 May 2026. Download (1MB) | Request a copy
	Text 03191038_paper.pdf Restricted to Repository staff only until 4 May 2026. Download (467kB) | Request a copy
	Text 03191038_presentation.pdf Restricted to Repository staff only until 4 May 2026. Download (3MB) | Request a copy
	Text Form. TA-020.pdf Restricted to Repository staff only until 4 May 2026. Download (66kB) | Request a copy

Abstract

An airfoil is a wide-profiled structure applied in various fields such as aircraft wings, wind turbines, jet engine compressor blades, propeller blades, hydrofoils, vertical stabilizers of aircraft, submarine fins, and rotaries. The shape of an airfoil can be either symmetric or asymmetric, as exemplified by the NACA 4412 airfoil from the National Advisory Committee for Aeronautics (NACA). This study aims to evaluate the maximum stress, deformation, and elastic shear strain values. The method employed in this research is Finite Element Analysis (FEA) simulation. The analysis reveals that the highest stress is recorded in the carbon fiber composite honeycomb airfoil type, reaching 30,703 MPa. Meanwhile, the maximum strain occurs in the carbon fiber composite honeycomb airfoil at 28.88 mm/mm, with the smallest deflection observed in the carbon fiber epoxy composite, measuring 3.8106 mm.

Item Type:	Thesis (Bachelor)
Subjects:	A General Works > AS Academies and learned societies (General) T Technology > T Technology (General)
Divisions:	Jurusan Teknologi Industri dan Proses > Teknik Mesin
Depositing User:	Hangduaril Charta Wijaya
Date Deposited:	27 Dec 2023 04:58
Last Modified:	27 Dec 2023 04:58
URI:	http://repository.itk.ac.id/id/eprint/20665

Actions (login required)

View Item