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A new hypersonic boundary layer facility
M. L. Baumgartner
, A. J. Smitst
, T. Nau
,
C. W. Rowley
Mechanical & Aerospace Engineering
Princeton Institute for Computational Science and Engineering
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Keyphrases
High Mach number
100%
Turbulence
100%
Hypersonic Boundary Layer
100%
Blowout
100%
Transition Waves
100%
Transition Shock
100%
SWBLI
100%
Physics
Mach Number
100%
Shock Wave
100%
Boundary Layer
100%
Hypersonic Boundary Layer
100%