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