
INFLUENCE OF BOUNDARY LAYER IN THR CROWN BLADE ON SPECIFICATIONS FOR DEGREE OF AXIAL COMPRESSOR
Author(s) -
I. Ластівка
Publication year - 2010
Publication title -
naukoêmnì tehnologìï/naukoêmni tehnologìï
Language(s) - English
Resource type - Journals
eISSN - 2310-5461
pISSN - 2075-0781
DOI - 10.18372/2310-5461.7.5239
Subject(s) - blade (archaeology) , degree (music) , boundary layer , crown (dentistry) , gas compressor , boundary (topology) , layer (electronics) , structural engineering , mechanical engineering , mathematics , geometry , engineering , materials science , aerospace engineering , physics , composite material , mathematical analysis , acoustics