Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods

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
Hauptverfasser: Aulchenko, S. M., Galkin, V. M., Zvegintsev, V. I., Shiplyuk, A. N.
Format: Artikel
Sprache:eng
Schlagworte:
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
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Beschreibung
Zusammenfassung: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.
ISSN:1062-0125
1573-871X
DOI:10.1007/s10891-010-0306-6