Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
2010 / 08 Vol. 224; Iss. 8
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The effect of upstream duct boundary layer growth and compressor blade lean angle variation on an axial compressor performance
Templalexis, I., Pachidis, V., Pilidis, P., Kotsiopoulos, P.Volume:
224
Language:
english
Journal:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
DOI:
10.1243/09544100jaero637
Date:
August, 2010
File:
PDF, 464 KB
english, 2010