PERANCANGAN APLIKASI
ADISUTJIPTO TURBINE GAS PERFORMANCE (ATAP)
BERBASIS MATLAB GRAPHICAL USER INTERFACE (GUI)
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
Daffa’ Anestya, Ahmad
Subject
T Technology (General)
Datestamp
2024-02-15 08:26:06
Abstract :
The engine is a very important component for an aircraft, because engine performance is one of the benchmarks in assessing the flight performance of an aircraft, the engine is also a benchmark in designing an aircraft. The performance of an aircraft engine can be measured by the value of specific fuel consumption, thrust produced, and efficiency, but in practice there are a series of calculations that are iterated to get the value of these output variables. In this research, the topic is to design an application called Adisutjipto Turbine Gas Performance (ATAP) which functions to be able to perform performance calculations on aircraft engines. The ATAP application is designed on the basis of Matlab GUI, and uses the main reference by Jack D. Mattingly with the title "Element of Gas turbine Propulsion" 2005 edition as the basis for the calculation. The ATAP design process is also assisted by Excel and the results of the calculation values and plotting will be compared with the calculation results in the main reference and from the pre-existing application called PARA. After the design and comparison, the results showed that the accuracy of the results obtained through plotting between iteration variables and output variables using ATAP is quite good. The plot produced by ATAP using the same data, has a good resemblance of the shape of the plot line and also the calculation value with the plot graph found in the main reference
The engine is a very important component for an aircraft, because engine performance is one of the benchmarks in assessing the flight performance of an aircraft, the engine is also a benchmark in designing an aircraft. The performance of an aircraft engine can be measured by the value of specific fuel consumption, thrust produced, and efficiency, but in practice there are a series of calculations that are iterated to get the value of these output variables. In this research, the topic is to design an application called Adisutjipto Turbine Gas Performance (ATAP) which functions to be able to perform performance calculations on aircraft engines. The ATAP application is designed on the basis of Matlab GUI, and uses the main reference by Jack D. Mattingly with the title "Element of Gas turbine Propulsion" 2005 edition as the basis for the calculation. The ATAP design process is also assisted by Excel and the results of the calculation values and plotting will be compared with the calculation results in the main reference and from the pre-existing application called PARA. After the design and comparison, the results showed that the accuracy of the results obtained through plotting between iteration variables and output variables using ATAP is quite good. The plot produced by ATAP using the same data, has a good resemblance of the shape of the plot line and also the calculation value with the plot graph found in the main reference
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