Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes /

Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes / Daniel L. Sutliff and Clifford A. Brown, Bruce E. Walker.

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Bibliographic Details
Online Access:	Online Access Online Access
Main Authors:	Sutliff, Daniel L. (Daniel Linden), 1962- (Author), Brown, Clifford A. (Clifford Alan) (Author), Walker, Bruce E. (Author)
Corporate Author:	Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
Series:	NASA technical memorandum ; 218119.
Subjects:	Acoustic properties. Aerodynamic configurations. Turbofan engines. Ducts. Aerodynamic noise. Wind tunnel tests.

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Call Number:	NAS 1.15:2014-218119
NAS 1.15:2014-218119	Available