Flow Inside a Solid Rocket Motor with Relation to Nozzle Inlet Ablation
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Kanagawa 229-8510, Japan
2. IHI Aerospace Engineering Company, Ltd., Gunma 370-2307, Japan
3. IHI Aerospace Company, Ltd., Gunma 370-2398, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.22952
Reference15 articles.
1. Rotational axisymmetric mean flow and damping of acoustic waves in asolid propellant rocket.
2. Flow Analysis of a Solid Propellant Rocket Motor with Aft Fins
3. Effects of grain and aft-dome configuration on aft-end SRB internal flows
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