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

Bibliographic Details
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Boldman, Donald R.
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, DC] : National Aeronautics and Space Administration, [1992?]
Series:	NASA technical memorandum ; 105935.
Subjects:	Propellers, Aerial. Angle of attack (Aerodynamics) Angle of attack. Flow velocity. Inlet flow. Separated flow. Shrouded propellers. Subsonic speed.
Online Access:	https://purl.fdlp.gov/GPO/LPS97761

Description
Item Description:	Microform.
Physical Description:	1 volume Also 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.