%0 Journal Article
%T A technique for calculating characteristics of axial flow compressor stage with blades of large relative length
%A Rzhavin, Yu.
%A Karasev, V.
%J Russian Aeronautics (Iz VUZ)
%V 56
%N 4
%P 414-417
%@ 1068-7998
%D 2014-03-13
%I Allerton Press
%~ DeepDyve