Integrated Fluid–Structure Simulation for Full Burning of a Solid-Propellant Rocket Interior
Author:
Affiliation:
1. School of Mechanical and Aerospace Engineering, Department of Aerospace Engineering, Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35107
Reference47 articles.
1. Flow-structural interaction inside a solid rocket motor during ignition transient
2. Solid Rocket Motor Internal Ballistics Simulation Using Three-Dimensional Grain Burnback
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5. Transient Burning Characteristics of JA2 Propellant Using Experimentally Determined Zel'dovich Map
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