DEVELOPMENT TESTING METHOD AND ANALYSIS FOR STATIC THRUST MEASUREMENT

New aircraft development has to be supported with system development such as avionic, electric, structure and propulsion. Propulsion system is one of importance thing to influence aircraft performance. Propulsion system development either machine or propeller involved aircraft manufacturer and engin...

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主要作者: Khasyofi, Mitra
格式: Theses
語言:Indonesia
在線閱讀:https://digilib.itb.ac.id/gdl/view/34917
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機構: Institut Teknologi Bandung
語言: Indonesia

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