Numerical Simulation of Axisymmetric Solid Rocket Motor Ignition Transient with Radiation Effect
Author:
Affiliation:
1. Korea Aerospace Research Institute, Yusung-ku, Taejon, 305-600, Republic of Korea
2. Korea Advanced Institute of Science and Technology, Gusung-dong, Yusung-ku, Taejon 305-701, 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/10.2514/2.5636
Reference7 articles.
1. Finite volume radiative heat transfer procedure for irregular geometries
2. Solid rocket motor internal flow during ignition
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2. Parametric Study on Solid Rocket Motor Ignition Transient and Pressure Oscillations Onset;Journal of Propulsion and Power;2015-07
3. 3D Flow Simulation of Dual Thrust Solid Rocket Motors during Starting Transient;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-25
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