Increased jet noise due to a "nominally laminar" state of nozzle exit boundary layer /

Bibliographic Details

Main Author:	Zaman, K. B. M. Q. (Khairul B. M. Q.) (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2017.
Series:	NASA technical memorandum ; 2017-219440.
Subjects:	Jet aircraft noise. Jet nozzles. Sound pressure. Subsonic flow. Turbulent boundary layer.
Online Access:	https://purl.fdlp.gov/GPO/gpo81483 http://purl.fdlp.gov/GPO/gpo81483