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. 1By:Duman, Serdar;Tunçer, OnurPublication type:Article