Works matching DE "AIRPLANE turbofan engine blades"
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QUASI THREE DIMENSIONAL COMPRESSOR DESIGN FOR A TWIN-SPOOL LOW BYPASS RATIO TURBOFAN ENGINE.
- Published in:
- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2012, v. 5, n. 3, p. 1
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- Publication type:
- Article