Computational approach in sizing of pulsejet engine

Research in pulsejet has intensified recently due to its design simplicity that can be developed into efficient small scale propulsive units for new applications such as UAVs and Unmanned Combat Vehicles (UCAV). A major obstacle for its development is low efficiency of the engine. The objective of t...

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Những tác giả chính: Ahmad, Mohamed Tarmizi, Ahmadian, Sevda, Md Zhahir, Md Amzari, Ariff, Omar Kassim, Romli, Fairuz Izzudin
Định dạng: Bài viết
Ngôn ngữ:English
Được phát hành: Trans Tech Publications 2014
Truy cập trực tuyến:http://psasir.upm.edu.my/id/eprint/36871/1/Computational%20approach%20in%20sizing%20of%20pulsejet%20engine.pdf