Optical characterization of a multipoint lean direct injector for gas turbine combustors : velocity and fuel drop size measurements /

Bibliographic Details
Corporate Authors:	NASA Glenn Research Center, ASME Turbo Expo
Other Authors:	Heath, Christopher M.
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216365.
Subjects:	Fuel injection. Gas turbines. Flight conditions. Computational fluid dynamics. Combustion chambers. Aircraft engines. Flame temperature. Inlet temperature. Supersonic flight.
Online Access:	https://purl.fdlp.gov/GPO/gpo6453

Description
Item Description:	Title from title screen (viewed on April 21, 2011). "October 2010." Electronic resource.
Physical Description:	1 online resource (13 pages) : illustrations, color
Bibliography:	Includes bibliographical references (page 13).