DESAIN DAN PEMBUATAN PANDUAN
PERAWATAN PESAWAT UAV FLYING WING
GO-DRONE STTA
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
FICHRI ABDULLAH, ILHAM
Subject
T Technology (General)
Datestamp
2024-07-23 06:45:56
Abstract :
Aerial photography is an indispensable job for companies which own lands such as mining, plantations, etc. UAV aircraft is a solution to assist in aerial photography work. Flying wing type UAV is one type of aircraft used for aerial photography. The purpose of this research is to produce design, geometry, aerodynamic characteristics and aircraft maintenance manual of UAV flying wing GO-DRONE STTA. In the process of this research, the method used for the design process is the analytical process of Raymer and Roskam. The method in the design process begins with determining the DRO, determining the weight, wing span, wing geometry. The result of the geometry that has been determined is drawn in 3 dimensional form using CATIA software. 3-dimensional image results are then analyzed to determine the aerodynamic characteristics of UAV aircraft using ANSYS software The results showed that the UAV aircraft obtained coefficient of lift force of 0.305 at the moment of attack angle 00. The value of the maximum lift coefficient of 1.028 at the time of the attack angle 150. The value of the drag coefficient at the attack angle 00 of 0.042. The maximum drag coefficient value is 0.604 when the attack angle is 300. The guided result is divided into pre flight inspection and after flight inspection and damage after manufacturing process.
Aerial photography is an indispensable job for companies which own lands such as mining, plantations, etc. UAV aircraft is a solution to assist in aerial photography work. Flying wing type UAV is one type of aircraft used for aerial photography. The purpose of this research is to produce design, geometry, aerodynamic characteristics and aircraft maintenance manual of UAV flying wing GO-DRONE STTA. In the process of this research, the method used for the design process is the analytical process of Raymer and Roskam. The method in the design process begins with determining the DRO, determining the weight, wing span, wing geometry. The result of the geometry that has been determined is drawn in 3 dimensional form using CATIA software. 3-dimensional image results are then analyzed to determine the aerodynamic characteristics of UAV aircraft using ANSYS software The results showed that the UAV aircraft obtained coefficient of lift force of 0.305 at the moment of attack angle 00. The value of the maximum lift coefficient of 1.028 at the time of the attack angle 150. The value of the drag coefficient at the attack angle 00 of 0.042. The maximum drag coefficient value is 0.604 when the attack angle is 300. The guided result is divided into pre flight inspection and after flight inspection and damage after manufacturing process.
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