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Analysis of grain burnback and international flow in solid propellant rocket motors in 3-dimensions
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index.pdf
Date
2007
Author
Yıldırım, Cengizhan
Metadata
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In this thesis, Initial Value Problem of Level-set Method is applied to solid propellant combustion to find the grain burnback. For the performance prediction of the rocket motor, 0-D, 1-D or 3-D flow models are used depending on the type of thre grain configuration.
Subject Keywords
Solid propellant rockets.
,
Mechanical engineering.
URI
http://etd.lib.metu.edu.tr/upload/2/12608283/index.pdf
https://hdl.handle.net/11511/17275
Collections
Graduate School of Natural and Applied Sciences, Theses
