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Monopropellant droplet decomposition for large activation energies
Citation
Liñán Martínez, Amable (1975). Monopropellant droplet decomposition for large activation energies. "Acta Astronautica", v. 2 (n. 11-12); pp. 1009-1029. ISSN 0094-5765.
Description
| Title: | Monopropellant droplet decomposition for large activation energies |
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| Author/s: |
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| Item Type: | Article |
| Título de Revista/Publicación: | Acta Astronautica |
| Date: | 1975 |
| ISSN: | 0094-5765 |
| Volume: | 2 |
| Subjects: | |
| Freetext Keywords: | ROCKETS AND MISSILES - Propellants; LIQUID FUELS |
| Faculty: | E.T.S.I. Aeronáuticos (UPM) |
| Department: | Motopropulsión y Termofluidodinámica [hasta 2014] |
| Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
Abstract
An asymptotic theory has been developed for the quasi-steady decompositon of a monopropellant droplet in a quiescent atmosphere, when the gas decompositon reaction is of the Arrhenius type, with an activation temperature E/R much larger than the characteristic gas temperature. By formulating the problem mathematically, it is shown how, in the limit of large activation energies, regions of near equilibrium flow or frozen flow may coexist in the flow field. The nearly frozen ignition regime is then analyzed, and complete decomposition and the partial decomposition regimes are presented.
More information
| Item ID: | 1005 |
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| DC Identifier: | https://oa.upm.es/1005/ |
| OAI Identifier: | oai:oa.upm.es:1005 |
| Official URL: | http://www.sciencedirect.com/science/journal/00945... |
| Deposited by: | Archivo Digital UPM |
| Deposited on: | 14 May 2008 |
| Last Modified: | 20 Apr 2016 06:38 |
