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Burning rate acceleration sensitivity of double-base propellant

✍ Scribed by BULMAN, M. J.; NETZER, D. W.


Book ID
119952015
Publisher
American Institute of Aeronautics and Astronautics
Year
1970
Tongue
English
Weight
358 KB
Volume
8
Category
Article
ISSN
0001-1452

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The burning rate of a hot double-base homogeneous solid propellant is modeled by the numerical solution of the conservation equations characterizing the primary flame using a global kinetic scheme. The increase of the burning rate above the solid surface is modeled by an enhancement of the heat tran