A Mach-Zehnder interferometer has been used for both flow-field visualization and quantitative assessment of aerodynamic parameters in a shock tube environment. Of special interest are the high- temperature effects in the post-shock region of bodies travelling at hypervelocity. Infinite-fringe interferograms give the density contours of the flow field and, in combination with an equilibrium real gas code, they can be used to provide information on the non-equilibrium state of the dissociating flow.
Visualization of non-equilibrium dissociating flows
1997-05-01
11 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Visualization of non-equilibrium dissociating flows
Online Contents | 1997
|Non-equilibrium laminar boundary-layer flow of dissociating air
Elsevier | 1975
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