Numerical Study of the Dynamic Characteristics of Pintle Nozzles for Variable Thrust
Author:
Affiliation:
1. School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 412-791, 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.B35257
Reference9 articles.
1. Solid propulsion approaches for terminal steering
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3. Numerical simulation of the flowfield inside a hot gas valve
4. KimJ. G. “Study on the Effects of Pintle Shapes and Position in Nozzle Flowfield, and Thrust in a Solid Rocket Motor with Pintle Nozzle,” Ph.D. Dissertation, Dept. of Mechanical Design Engineering, Chungnam National Univ., Daejeon, ROK, 2011.
5. Investigation of Pintle Shape Effect on the Nozzle Performance
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