Abstract
It is experimentally established that gas-permeable inserts arranged in front of a finite rectangular step can reduce the characteristic size of the recirculation region for oncoming flow with Mach numbers within M = 2–5.
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Original Russian Text © V.M. Fomin, B.V. Postnikov, K.A. Lomanovich, 2015, published in Pis’ma v Zhurnal Tekhnicheskoi Fiziki, 2015, Vol. 41, No. 18, pp. 68–73.
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Fomin, V.M., Postnikov, B.V. & Lomanovich, K.A. Changing the regime of supersonic flow past a rectangular step using gas-permeable inserts. Tech. Phys. Lett. 41, 898–900 (2015). https://doi.org/10.1134/S1063785015090205
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DOI: https://doi.org/10.1134/S1063785015090205