CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report /

Saved in:

Bibliographic Details
Author / Creator:	Vinci, Samuel J., author.
Imprint:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2012.
Description:	1 online resource (xiv, 113 pages) : color illustrations.
Language:	English
Series:	NASA/CR ; 2012-217417 NASA contractor report ; NASA CR-2012-217417.
Subject:	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/10756024

Hidden Bibliographic Details
Varying Form of Title:	Computational fluid dynamics simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A)
Other authors / contributors:	Cleveland State University. Fundamental Aeronautics Program (U.S.), sponsoring body. NASA Glenn Research Center, issuing body.
Notes:	Title from title screen (viewed Nov. 24, 2015). "September 2012." "Performing organization: Cleveland State University"--Report documentation page. "Prepared under NASA interagency agreement no. NNC07IA10I (through U.S. Navy Agreement No. N00189-07-P-A253)." Includes bibliographical references (pages 110-113). Final contractor report; January 2007 to September 2010. Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center NNC07IA10I N00189-07-P-A253 DE-FC26-06NT42853 WBS 561581.02.08.03.47.02.01 E-18088
GPO item no.:	0830-H-14 (online)
Govt.docs classification:	NAS 1.26:2012-217417

Similar Items