Numerical simulations of two-phase reacting flow in a single-element lean direct injection (LDI) combustor using NCC /

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Bibliographic Details
Author / Creator:Liu, Nan-Suey.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Description:1 online resource (28 p.) : col. ill.
Language:English
Series:NASA/TM ; 2011-217031
NASA technical memorandum ; 217031.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8623258
Hidden Bibliographic Details
Other authors / contributors:Shih, Tsan-Hsing, 1940-
Wey, C. Thomas.
Fundamental Aeronautics Program (U.S.)
NASA Glenn Research Center.
Notes:Title from title screen (viewed on Jan. 9, 2012).
"July 2011."
Includes bibliographical references (p. 9-10).
E-17725
Sponsored by the Fundamental Aeronautics Program WBS 561581.02.08.03.16.02
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2011-217031