QUASI THREE DIMENSIONAL COMPRESSOR DESIGN FOR A TWIN-SPOOL LOW BYPASS RATIO TURBOFAN ENGINE.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2012, v. 5, n. 3, p. 1
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Works matching DE "AIRPLANE turbofan engine design %26 construction"
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Effectiveness of combined aircraft engine noise suppressors.
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- Acoustical Physics, 2012, v. 58, n. 4, p. 510, doi. 10.1134/S1063771012040094
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