Transition within a Hypervelocity Boundary Layer on a 5-degree Half-Angle Cone in Freestream Air/CO2 Mixtures

The most significant instability mechanism which leads to laminar to turbulent transition in hypervelocity flow over cold, slender bodies, characteristic of high enthalpy facilities like the T5 hypervelocity shock tunnel at Caltech, is the so-called second or Mack mode, which depends upon the amplic...

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Hauptverfasser:	Jewell, Joseph S, Wagnild, Ross M, Leyva, Ivett A, Candler, Graham V, Shepherd, Joseph E
Format:	Report
Sprache:	eng
Schlagworte:	ANGLE OF ATTACK BOUNDARY LAYER ENTHALPY Fluid Mechanics FREE STREAM INVISCID FLOW LOW TEMPERATURE MACH NUMBER REYNOLDS NUMBER SHOCK TUNNELS SLENDER BODIES TRAPPING(CHARGED PARTICLES) VISCOSITY
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