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

Bibliographic Details

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.
Online Access:	https://purl.fdlp.gov/GPO/gpo53741 http://purl.fdlp.gov/GPO/gpo53741