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Download full textBulat, Pavel V.; Volkov, Konstantin N. – International Journal of Environmental and Science Education, 2016
In this article we reviewed the shock wave oscillation that occurs when supersonic flows interact with conic, blunt or flat nose of aircraft, taking into account the aerospike attached to it. The main attention was paid to the problem of numerical modeling of such oscillation, flow regime classification, and cases where aerospike attachment can…
Descriptors: Air Transportation, Classification, Fuels, Accuracy
