29th International Symposium on Shock Waves 1 2015
DOI: 10.1007/978-3-319-16835-7_80
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Visualization of Hypersonic Flat-Plate Boundary Layer in Shock Tunnel

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Cited by 1 publication
(2 citation statements)
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“…Then, the first Fresnel radius F 1 is deduced as Figure 4. The image of the flat-plate boundary layer using nanoparticle-based planar laser scattering, which is the result given in Zhang et al (2015). Note that the dash lines are not included in the original picture, which are added for conveniently describing in this paper.…”
Section: Radio Sciencementioning
confidence: 99%
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“…Then, the first Fresnel radius F 1 is deduced as Figure 4. The image of the flat-plate boundary layer using nanoparticle-based planar laser scattering, which is the result given in Zhang et al (2015). Note that the dash lines are not included in the original picture, which are added for conveniently describing in this paper.…”
Section: Radio Sciencementioning
confidence: 99%
“…The smooth degree of the interfaces can be qualitatively displayed by simulating the supersonic airflow structure. Figure 4 is the result given in Zhang et al (2015), which aimed at investigating the transition process in supersonic turbulent area. Note that the dash lines are not included in the original figure and are added for conveniently illustrating in this paper.…”
Section: Radio Sciencementioning
confidence: 99%