Mainil Afdhal, Kurniawan (2011) ANALISA KINERJA ENGINE TURBOFAN CFM56-3. Jurnal Teknik Mesin, 8 (2). pp. 78-82. ISSN 1829-8958

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This study focused on the performance analysis of a turbofan engine type used on commercial aircraft with CFM56-3 type. The performance tests consisted of several stages of testing are the the start up testing phase, the minimum idle, the idle approach, the maximum continuous, the take off, and the acceleration. Each of test has the characteristics, so the working, efficiency, and thrust at each condition are different. In order to obtain comparisons between each condition, the Brayton cycle was used as a reference, then the actual work and the ideal, the cycle thermal efficiency and engine thrust from each test condition can be known. The highest thermal efficiency was achieved on the actual take off condition with an efficiency of 37% while the ideal is 47%, for the actual thrust of 2397.43873 lb while the ideal is 25091.96387 lb.

Item Type: Article
Subjects: T Technology > TJ Mechanical engineering and machinery
Divisions: Unspecified > Journal
Depositing User: 001 Bambang Gonggo Murcitro
Date Deposited: 02 Mar 2013 00:10
Last Modified: 05 May 2013 01:07

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