SIMULASI KEKUATAN STRUKTUR WING UAV VTOL SKYBEEJO V1

Gilang Saputra, Alfin (2024) SIMULASI KEKUATAN STRUKTUR WING UAV VTOL SKYBEEJO V1. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

	Text (ABSTRAK) 19050094_ABSTRAK.pdf Download (31kB)
	Text (BAB I) 19050094_BAB 1.pdf Download (40kB)
	Text (DAFTAR PUSTAKA) 19050094_DAFTAR PUSTAKA.pdf Download (145kB)
	Text (FULL SKRIPSI) 19050094 - converted.pdf Restricted to Repository staff only Download (721kB)

Abstract

Utilization of drones includes monitoring urban spatial planning, observing forest areas. Skybeejo is one type of fixed-wing UAV owned by CV Archapada Raya. Fixed-wing UAVs cannot take off and land on narrow runways. Therefore, modifications were made to this aircraft from the previous conventional method of takeoff and landing to VTOL (Vertical Takeoff and Landing). Consequently, changes are required in the type of material and geometry to be used in the wing structure. Thus, this study focuses on simulating the strength of the wing structure using carbon fiber and balsa wood as the primary materials to determine the safety of the structure based on the margin of safety. The results show that the half-span geometry is 1325mm with 14 ribs. The maximum stress occurs during maneuver loading at 22.354 MPa, during negative limit loading at 16.785 MPa, and during VTOL loading at 15.176 MPa. The failure criteria and margin of safety indicate that the structure is safe.

Actions (login required)

View Item

Downloads