A non-cut cell immersed boundary method for use in icing simulations /

Saved in:

Bibliographic Details
Author / Creator:	Sarofeen, Christian M., author.
Imprint:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
Description:	1 online resource (31 pages) : illustrations (some color).
Language:	English
Series:	NASA/TM ; 2013-217881 NASA technical memorandum ; 2013-217881.
Subject:	Aerodynamic coefficients. Aerodynamic drag. Computational fluid dynamics. Control surfaces. Finite volume method. Ice formation. Pressure distribution. Computational fluid dynamics. Finite volume method.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/9977515

Hidden Bibliographic Details
Other authors / contributors:	Noack, Ralph W., author. Kreeger, Richard E., author. NASA Glenn Research Center, issuing body. United States. National Aeronautics and Space Administration, sponsoring body.
Notes:	Title from title screen (viewed on Apr. 9, 2014). "July 2013." "Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Nashville, Tennessee, January 9-12, 2012." "AIAA-2012-1204." Includes bibliographical references (page 31). Sponsored by National Aeronautics and Space Administration NNX08AW92A WBS 877868.02.07.03.03.01 E-18692
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:2013-217881

Similar Items