1967
DOI: 10.21236/ad0819547
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Comparison of Theoretical and Experimental Pressure and Heat-Transfer Distributions on Three Blunt Nosed Cylinders in Hypersonic Flow

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Cited by 5 publications
(4 citation statements)
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“…This type of separation is called shoulder separation as described in Kaufman II et al (1966), which is caused by an adverse pressure gradient because of recompressions of the flow after a strong expansion. Such a separation on cylinder's shell surface was also observed in Matthews and Eaves Jr. (1967).…”
Section: Experimental and Computational Flow Visualizationsupporting
confidence: 64%
“…This type of separation is called shoulder separation as described in Kaufman II et al (1966), which is caused by an adverse pressure gradient because of recompressions of the flow after a strong expansion. Such a separation on cylinder's shell surface was also observed in Matthews and Eaves Jr. (1967).…”
Section: Experimental and Computational Flow Visualizationsupporting
confidence: 64%
“…The experimental results in [15] showed that beyond a certain Reynolds number (between 148 × 10 3 and 549 × 10 3 ), the strong expansion around the windward edges of a cube can cause a breakaway or shoulder separation to form. This behaviour has also been observed in hypersonic flows around cylinders [9] and 2D shapes [12]. Due to the orientation of the model in these experiments, the schlieren images (Figure 11) do not capture the density variations (such as separation and re-attachment shocks) associated with such a separation.…”
Section: Flow Structures: Schlieren Images Mach Contours and Vortex V...mentioning
confidence: 70%
“…We also note that earlier studies [9] of the hypersonic heat fluxes in the region immediately downstream of a strong expansion corner found it very challenging to measure the heat flux in this region, possibly due to the extreme sensitivity of the flow in this region to the Reynolds number.…”
Section: Differences Between Cfd and Experimentsmentioning
confidence: 88%
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