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Monopropellant droplet decomposition for large activation energies

Liñán Martínez, Amable (1975) Monopropellant droplet decomposition for large activation energies. Acta Astronautica, 2 (11-12). pp. 1009-1029. ISSN 0094-5765

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Item Type:Article
Authors/Creators:
Creators NameCreators email (if known)
Liñán Martínez, Amable
Title:Monopropellant droplet decomposition for large activation energies
Journal/Publication Title:Acta Astronautica
Date:1975
Volume:2
Number:11-12
Department:Motopropulsión and thermofluidynamic
Faculty:E.T.S.I. Aeronautical (UPM)
Creative Commons licenses:Recognition - No derivative works - No commercial
Item ID:1005
Subjects:Mathematics
Physics

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Official URL: http://www.sciencedirect.com/science/journal/00945765

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.

Item Type:Article
Uncontrolled Keywords:ROCKETS AND MISSILES - Propellants; LIQUID FUELS
Subjects:Mathematics
Physics
Código ID:1005
Depositado Por:Archivo Digital UPM
Depositado el:14 May 2008
Last Modified:23 Sep 2009 18:42

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