Numerical Investigation of Tandem Airfoils for Subsonic Axial-Flow Compressor Blades
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, VA
2. Rolls-Royce Corporation, Indianapolis, IN
Abstract
Publisher
ASMEDC
Link
http://asmedigitalcollection.asme.org/IMECE/proceedings-pdf/doi/10.1115/IMECE2007-43929/4555917/53_1.pdf
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