Multisized Inert Particle Loading for Solid Rocket Axial Combustion Instability Suppression

In the present investigation, various factors and trends, related to the usage of two or more sets of inert particles comprised of the same material (nominally aluminum) but at different diameters for the suppression of axial shock wave development, are numerically predicted for a composite-propella...

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Bibliographic Details
Main Author: David R. Greatrix
Format: Article
Language:English
Published: Wiley 2012-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2012/173129
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