Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Pedro Paredes (Langley Research Center Hampton, Virginia, United States) Meelan M Choudhari (Langley Research Center Hampton, Virginia, United States) Fei Li (Langley Research Center Hampton, Virginia, United States) Chau-Lyan Chang (Langley Research Center Hampton, Virginia, United States) Date Acquired
January 17, 2017
Publication Date
June 17, 2016
Publication Information
Publication: AIAA Journal
Publisher: American Institute of Aeronautics and Astronautics
Volume: 54
Issue: 10
Issue Publication Date: October 1, 2016
ISSN: 0001-1452
e-ISSN: 1533-385X
Subject Category
Fluid Mechanics And Thermodynamics Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Compressible boundary layerFreestream Mach NumberShock layersLeading edgesIncompressible flowNavier Stokes equationsEnthalpyParabolized stability equationsKinetic energyCompressibility effect