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Results of an advanced fan stage operating over a wide range of speed and bypass ratio Kenneth L. Suder [and five others].

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Format:
Book
Conference/Event
Government document
Author/Creator:
Suder, Kenneth L. (Kenneth Lee)
Contributor:
Fundamental Aeronautics Program (U.S.), sponsoring body.
NASA Glenn Research Center, issuing body.
Conference Name:
ASME Turbo Expo (2010 : Glasgow, Scotland, U.K.)
Series:
NASA technical memorandum ; 216769.
NASA/TM ; 2010-216769, 2011-216769
Language:
English
Subjects (All):
Computational fluid dynamics.
Physical Description:
1 online resource (2 volumes) : color illustrations.
Place of Publication:
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]-[2011]
Contents:
pt. 1. Fan stage design and experimental results
pt 2. Comparison of CFD and experimental results.
Notes:
Title from title screen (viewed on Jan. 29, 2014).
"Prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010."
Includes bibliographical references.
OCLC:
707645081

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