Determination of the operating characteristics of a variable mach number supersonic wind tunnelCopyright 漏 is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public ...
Plasma physics Numerical investigation of the nonlinear transition regime in supersonic boundary layers THE UNIVERSITY OF ARIZONA Hermann F. Fasel MayerChristian S. JThe nonlinear transition regime of supersonic boundary layers at low to moderate supersonic Mach numbers (Mach 2-3.5) under wind-tunnel...
The additional advantage of no need for special apparatus, except for the infrared camera, makes IRT well suited for both wind-tunnel and in-flight testing. Practical problems and limitations encountered when dealing with IRT in high-speed flows are also discussed.doi:10.1007/s00348-007-0384-1...