ANALISIS TUMBUKAN PADA SAYAP PESAWAT TANPA AWAK JENIS SAYAP TETAP

HANIF, FADHILAH and Yani, Irsyadi (2018) ANALISIS TUMBUKAN PADA SAYAP PESAWAT TANPA AWAK JENIS SAYAP TETAP. Undergraduate thesis, Sriwijaya university.

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Abstract

This depth of study will contribute to the occurrence of maintenance at a time when it grows with the bar using the 2019 autodesk inventor Software. So it is necessary in the field of insurance for non-maintenance is very important because of important roles in human life, but some factors that affect the vehicle when it is in the air. From this analysis, it was done to identify the impact on the object on the case. In this Software analysis phase is autodesk inventor 2019, this analysis aims to reduce the risk that occurs when the machine collapses and knows the effect that occurs when it collapses with the frame. The aircraft can not be controlled by itself and can be reversed from a distance away and can be used as usual with the program being entered. The model used in the simulation uses the digital image to be fixed. In particular, the wing is made in the form of an airfoil that has been designed so well as to damage the required level, especially when the mirror covers the speed of a certain speed. The plane is modified by the air in the air air and is still moving with the power source produced from propellers or jet engines. Knowing the impact on various materials has a considerable benefit in the engineering field, for the material used acrylonitrile boutadine styrene (ABS) which has a Chemical, hard, can be designed to be some form, and is resistant to. In the simulation it is used and used in Computer devices using numerical Systems, and data collection is carried out statistically to obtain characteristics of the system. This analysis is derived from literature studies where writing searches for the ffequency of support in this study, but the design of the mosque is designed to be designed as an emergency. After designing it, it is made, then the next phase is carried out simulating it on the wing with the bar as a collision. And continued with testing and data collection in order to get results from the research that has been done. The discussion that will be carried out on the simulation finds out how the treatment is done without loss from the previous frequency. then do the analysis with the sum of 1000000N in the bars that are directed directly in the care section. then the style given gives the result of a pressure of 1217 MPa. And also the design of the wing model experienced in the color changes caused by the impact. The conclusions obtained from this study have been made, aiming to see that a number of collisions occur after 1000,000N and the result of the pressure obtained is 1217 MPa, and it appears that the largest part of the collision is in the maintenance section Keywords : Autodesk Inventor 2019, Analysis of Stasic, Fixed Wing, impact, static stress

Item Type:	Thesis (Undergraduate)
Uncontrolled Keywords:	Tumbukan, Sayap Pesawat, Awak Pesawat
Subjects:	T Technology > TJ Mechanical engineering and machinery > TJ241-254.7 Machine construction (General) > TJ241.I59 Machine design--Congresses. Production engineering--Congresses
Divisions:	03-Faculty of Engineering > 21201-Mechanical Engineering (S1)
Depositing User:	Ichlasyah Aisyah
Date Deposited:	11 Aug 2025 04:04
Last Modified:	11 Aug 2025 04:04
URI:	http://repository.unsri.ac.id/id/eprint/182662

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