On the basis of the solution of direct problems with the use of various medium models and numerical methods of integration of gas flow equations, methods for designing super- and hypersonic nozzles have been developed. Multimode nozzles in the ranges of Mach numbers 8–14 and 14–20 satisfying given conditions have been designed.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 82, No. 6, pp. 1109–1112, November–December, 2009.
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Aulchenko, S.M., Galkin, V.M., Zvegintsev, V.I. et al. Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods. J Eng Phys Thermophy 82, 1127–1131 (2009). https://doi.org/10.1007/s10891-010-0306-6
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DOI: https://doi.org/10.1007/s10891-010-0306-6