Investigation of active flow control to improve aerodynamic performance of oscillating wings /

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Bibliographic Details
Author / Creator:Narducci, Robert P., author.
Imprint:Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014.
Description:1 online resource (vi, 66 pages) : illustrations (some color).
Language:English
Series:NASA/CR ; 2014-218146
NASA contractor report ; NASA CR-2014-218146.
Subject:Aerodynamic stalling.
Computational fluid dynamics.
Active control.
Aerodynamic characteristics.
Rotary wing aircraft.
Boundary layer control.
Mach number.
Boundary layer control.
Computational fluid dynamics.
Mach number.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10293853
Hidden Bibliographic Details
Other authors / contributors:Langley Research Center, issuing body.
Notes:Title from title screen (viewed Oct. 9, 2014).
"January 2014."
Includes bibliographical references (page 53).
Sponsored by National Aeronautics and Space Administration NNL13AA03C 380046.02.07.03.02.02
GPO item no.:0830-H-14 (online)
Govt.docs classification:NAS 1.26:2014-218146
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