Aeromechanics analysis of a boundary layer ingesting fan /

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Bibliographic Details
Author / Creator:	Bakhle, Milind A., author.
Imprint:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
Description:	1 online resource (15 pages) : color illustrations.
Language:	English
Series:	NASA/TM ; 2013-217730 NASA technical memorandum ; 217730.
Subject:	Computational fluid dynamics. Dynamic loads. Propulsion system configurations. Inlet flow. Propulsion system performance. Reynolds averaging. Computational fluid dynamics.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10292971

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Other authors / contributors:	NASA Glenn Research Center, issuing body. Fundamental Aeronautics Program (U.S.), sponsoring body. United States. National Aeronautics and Space Administration.
Notes:	Title from title screen (viewed on Aug. 25, 2014). "January 2013." "Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Atlanta, Georgia, July 30-August 1, 2012." Includes bibliographical references (page 15). Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center WBS 561581.02.08.03.47.03.01 AIAA Paper 2012-3995 E-18442
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:2013-217730

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