The Reduction of Chemical Kinetic Mechanisms in High-Temperature Heterogeneous Flows in a Nozzle-Reference-Cited by-同舟云学术

The Reduction of Chemical Kinetic Mechanisms in High-Temperature Heterogeneous Flows in a Nozzle

Published:2021-01-04 Issue: Volume: Page:
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Container-title:AIAA Scitech 2021 Forum
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Author:

Naoumov Viatcheslav I.¹,Krioukov Viktor²,Abdullin Airat³

Affiliation:

1. Central Connecticut State University

2. Kazan National Research Technical University

3. Academy of Sciences of the Republic of Tatarstan

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. Chemical Kinetics in Combustion and Reactive Flows

2. Accurate Spatial Resolution Estimates for Reactive Supersonic Flow with Detailed Chemistry

3. Chemical Nonequilibrium, Heat Transfer, and Friction in a Detonation Tube with Nozzles

4. Гидаспов В.Ю. Северина Н.С. "Моделирование детонации металлогазовых горючих смесей в высокоскоростном потоке за ударной волной". Теплофизика высоких температур. 2019. Т. 57. № 4, cтр. 560-571. [Gidaspov V.Yu., Severina N.S. Modelling of Detonation of Metal-Gaseous Propellant Mixtures in the High-Temperature Flow Downstream of Shock Wave". High Temperature Journal, 2019, V. 57, N 4, pp. 560-571.]

5. Милёхин Ю.М. Попов В.С. Бурский Г.В. Гусев С.А. Садовничий Д.Н. "Моделирование связанных газотермодинамических процессов в ракетно-прямоточных двигателях на твердом топливе с учетом кинетики химических реакций. Часть 1. Постановка задачи" Известия Российской академии ракетных и артиллерийских наук. 2019. № 2 (107). стр. 51-57. [Milekhin Yu. M., Popov V.S., Burski G.V., Gusev S.A., Sadovnichiy D.N. "Modeling of Coupled Gas-Thermodynamic Processes in Solid-Propellant Ramjet Engines Allowing Kinetics of Chemical Reactions. Patrt 1. Statement of the Problem". Proceedings of theRussian Academy of Missile and Artillery Sciences, 2019. N 2 (107), pp.51-57]