2012
DOI: 10.3103/s8756699012030132
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Study of shock-wave flows in the channel by schlieren and background oriented schlieren methods

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Cited by 8 publications
(5 citation statements)
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“…Supersonic facilities such as shock tubes have also been used in order to visualize the shock-heated regions on a sharp cone at Mach 3.8 (Raghunath et al 2004) and shock waves at Mach 4 (Mizukaki 2010). Transonic flows and the shock waves contained have been examined by Glazyrin et al (2012) and Znamenskaya et al (2012). Wake flows behind wind tunnel models have been investigated in case of thermal, centrifugal and compressible effects.…”
Section: Bos Applications In Complex Facilitiesmentioning
confidence: 99%
“…Supersonic facilities such as shock tubes have also been used in order to visualize the shock-heated regions on a sharp cone at Mach 3.8 (Raghunath et al 2004) and shock waves at Mach 4 (Mizukaki 2010). Transonic flows and the shock waves contained have been examined by Glazyrin et al (2012) and Znamenskaya et al (2012). Wake flows behind wind tunnel models have been investigated in case of thermal, centrifugal and compressible effects.…”
Section: Bos Applications In Complex Facilitiesmentioning
confidence: 99%
“…where α is the angle of the direction of the ray with respect to the optical axis, and s o is the distance between the principal plane (the plane of lens and aperture) and the background. In practice, A ≈ 1 − 50 × 10 −3 m and s o ≈ 0.1 − 100 m. 7 For the paraxial approximation to be applicable within an accuracy of 1% (α < 15 • ≈ 0.25 rad), the relationship between r b and s o is…”
Section: Sensitivitymentioning
confidence: 99%
“…r t = r b + α s t is the distance of the deflecting point T from the optical axis, s t is the distance between the background and the test section (see figure 7 There are examples of using BOS technique for visualizing open air blast waves with so ≈ 400 m and st ≈ 100 m (Mizukaki et al 2012).…”
Section: Sensitivitymentioning
confidence: 99%
“…The authors of [100] used BOS together with PIV for combined visualization of a flow with a Mach number M = 8 in a wind tunnel. BOS studies of unsteady transonic flows containing shock waves in the channel and at the exit from the shock tube channel were carried out at Lomonosov Moscow State University ( [101,102]. Figure 16 shows 3 BOS images of the shock wave exit and the flow from the shock tube end.…”
Section: Background Oriented Schlieren Methodsmentioning
confidence: 99%
“…The effect recorded at the shock fronts often does not correlate with the physical parameters of the flow. In papers [107], [101] it was shown that this problem is actually caused by the fact that the detected value of refraction goes beyond the sensitivity of the method. Due to the strong light refraction at the shock front, the deflected beam can go beyond the optical scheme and not be detected.…”
Section: Background Oriented Schlieren Methodsmentioning
confidence: 99%