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E-REPORT
Title Secondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone / Fei Li [and three others].
Imprint Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2015.

Copies/Volumes

LOCATION CALL # STATUS
 Internet  Electronic Report    AVAILABLE
Description 1 online resource (24 pages) : color illustrations.
Series NASA/TM ; 2015-218997.
NASA technical memorandum ; 2015-218997.
Note Title from title screen (viewed April 26, 2016).
"December 2015."
"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
Bibliog. Includes bibliographical references (pages 20-24).
Note Sponsored by the National Aeronautics and Space Administration 109492.02.07.01.01.
L-20650.
Subject Boundary layer flow.
Circular cones.
Cross flow.
Hypersonic boundary layer.
Vortices.
Other Author Langley Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.