Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods
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 c...
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| Veröffentlicht in: | Journal of engineering physics and thermophysics 2009-11, Vol.82 (6), p.1127-1131 |
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| container_issue | 6 |
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| container_title | Journal of engineering physics and thermophysics |
| container_volume | 82 |
| creator | Aulchenko, S. M. Galkin, V. M. Zvegintsev, V. I. Shiplyuk, A. N. |
| description | 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. |
| doi_str_mv | 10.1007/s10891-010-0306-6 |
| format | Article |
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| ispartof | Journal of engineering physics and thermophysics, 2009-11, Vol.82 (6), p.1127-1131 |
| issn | 1062-0125 1573-871X |
| language | eng |
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| source | Springer Nature - Complete Springer Journals |
| subjects | Classical Mechanics Complex Systems Engineering Engineering Thermodynamics Gas flow Heat and Mass Transfer Hydrogasdynamics in Technological Processes Hypersonic nozzles Industrial Chemistry/Chemical Engineering Mach number Mathematical analysis Mathematical models Methods Nozzles Numerical analysis Optimization Thermodynamics |
| title | Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods |
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