Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets /

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Bibliographic Details
Imprint:	[Washington, DC] : National Aeronautics and Space Administration, [1992?]
Description:	1 volume.
Language:	English
Series:	NASA technical memorandum ; 105935 NASA technical memorandum ; 105935.
Subject:	Propellers, Aerial. Angle of attack (Aerodynamics)
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/7243881

Hidden Bibliographic Details
Other authors / contributors:	Boldman, Donald R. United States. National Aeronautics and Space Administration.
Notes:	Available via Internet from the NTRS web site. Address as of 07/22/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930007436%5F1993007436.pdf ; current access is available via PURL.
GPO item no.:	0830-D (MF) 0830-D (online)
Govt.docs classification:	NAS 1.15:105935

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