Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan /

Bibliographic Details
Main Author:	Herrick, Gregory Paul, 1972-
Corporate Authors:	Fundamental Aeronautics Program (U.S.), NASA Glenn Research Center, AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Series:	NASA technical memorandum ; 216959.
Subjects:	Aeroelasticity. Turbomachinery. Turbofans. Computational fluid dynamics. Inlet flow. Aerodynamic characteristics. High speed.
Online Access:	https://purl.fdlp.gov/GPO/gpo9159

Description
Item Description:	Title from title screen (viewed on June 27, 2011). "January 2011." "AIAA-2010-6711." Electronic resource.
Physical Description:	1 online resource (14 pages) : color illustrations
Bibliography:	Includes bibliographical references (pages 13-14).