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...
Saved in:
| 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 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations
by: David R. Greatrix
Published: (2008-01-01) -
Chemical Rocket Propulsion
by: David Greatrix, et al.
Published: (2012-01-01) -
Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine
by: Jianxiu Qin, et al.
Published: (2020-01-01) -
Effects of LOX Particle Diameter on Combustion Characteristics of a Gas-Liquid Pintle Rocket Engine
by: Xuan Jin, et al.
Published: (2020-01-01) -
Effect of Bluff Body Attributes on Afterburner Combustion Characteristics of a Boron Solid Rocket Scramjet
by: Jiang Ling, et al.
Published: (2024-01-01)