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Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations
Author
Source
International Journal of Aerospace Engineering
Issue
Vol. 2008, Issue 2008 (31 Dec. 2008), pp.1-10, 10 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2007-09-24
Country of Publication
Egypt
No. of Pages
10
Main Subjects
Engineering Sciences and Information Technology
Abstract EN
A general numerical model based on the Zeldovich-Novozhilov solid-phase energy conservation result for unsteady solid-propellant burning is presented in this paper.
Unlike past models, the integrated temperature distribution in the solid phase is utilized directly for estimating instantaneous burning rate (rather than the thermal gradient at the burning surface).
The burning model is general in the sense that the model may be incorporated for various propellant burning-rate mechanisms.
Given the availability of pressure-related experimental data in the open literature, varying static pressure is the principal mechanism of interest in this study.
The example predicted results presented in this paper are to a substantial extent consistent with the corresponding experimental firing response data.
American Psychological Association (APA)
Greatrix, David R.. 2007. Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations. International Journal of Aerospace Engineering،Vol. 2008, no. 2008, pp.1-10.
https://search.emarefa.net/detail/BIM-501186
Modern Language Association (MLA)
Greatrix, David R.. Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations. International Journal of Aerospace Engineering No. 2008 (2008), pp.1-10.
https://search.emarefa.net/detail/BIM-501186
American Medical Association (AMA)
Greatrix, David R.. Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations. International Journal of Aerospace Engineering. 2007. Vol. 2008, no. 2008, pp.1-10.
https://search.emarefa.net/detail/BIM-501186
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-501186