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).
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."
Includes bibliographical references (page 31).
Sponsored by National Aeronautics and Space Administration NNX08AW92A WBS 877868.
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2013-217881