ISSN:
1432-0649
Keywords:
07.60
;
42.80
;
82.80
Source:
Springer Online Journal Archives 1860-2000
Topics:
Physics
Notes:
Abstract Rotational temperature and nitrogen number density are measured in the shock wave/boundary layer interaction region in the vicinity of a two-dimensional compression corner disposed in a low pressure, 55 K, Mach 10 hypersonic air flow. Spatially-resolved data are recorded using a nonlinear optical technique named dual-line coherent anti-Stokes Raman scattering (DLCARS). Averaged temperature and density profiles are compared with those predicted by a Navier-Stokes solver. Good agreement is found.
Type of Medium:
Electronic Resource
URL:
http://dx.doi.org/10.1007/BF00332148
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