Mathematical simulation of hydrogen–oxygen combustion in rocket engines using LOGOS code
| Autor: | V. F. Nikitin, A.V. Sarazov, A. S. Kozelkov, I.M. Belyakov, R.M. Shagaliev, V.B. Betelin, S.V. Aksenov, Yu.N. Deryuguin, D. K. Zelenskiy, D.A. Korchazhkin |
|---|---|
| Rok vydání: | 2014 |
| Předmět: |
Engineering
business.product_category ComputerSystemsOrganization_COMPUTERSYSTEMIMPLEMENTATION Hydrogen business.industry Aerospace Engineering chemistry.chemical_element computer.software_genre Supercomputer Combustion law.invention Ignition system chemistry Rocket law Code (cryptography) Computer Aided Design Aerospace engineering business computer Verification and validation |
| Zdroj: | Acta Astronautica. 96:53-64 |
| ISSN: | 0094-5765 |
| Popis: | Hydrogen–oxygen fuels are very attractive now for rocket engines designers, because this pair is ecology friendly. Computer aided design of new effective and clean hydrogen engines needs mathematical tools for supercomputer modeling of hydrogen–oxygen components mixing and combustion in rocket engines. The paper presents the results of developing, verification and validation of mathematical model making it possible to simulate unsteady processes of ignition and combustion in rocket engines. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
|
Full Text from ScienceDirect