Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector /

Saved in:

Bibliographic Details
Author / Creator:	He, Zhuohui J., author.
Imprint:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
Description:	1 online resource (7 pages) : color illustrations.
Language:	English
Series:	NASA/TM ; 2014-218117 NASA technical memorandum ; 2014-218117.
Subject:	Combustion chambers. Nitrogen oxides.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10297457

Hidden Bibliographic Details
Other authors / contributors:	NASA Glenn Research Center, issuing body. Fundamental Aeronautics Program (U.S.), sponsoring body.
Notes:	Title from title screen (viewed on March 25, 2015). "April 2014." "Prepared for the 8th U.S. National Combustion Meeting sponsored by the Western State Section, Combustion Institute, Park City, Utah, May 19-22, 2013." Includes bibliographical references (page 7). Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center WBS 794072.02.03.05.02 E-18859
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:2014-218117

Similar Items