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Two-phase flow characteristics of solid rocket motors

Author: ZhangXu
Tutor: ZuoYe
School: Harbin Engineering University
Course: Aerospace Propulsion Theory and Engineering
Keywords: Gas-solid flow Equations Particle trajectory model Propellant
CLC: V435
Type: Master's thesis
Year: 2006
Downloads: 376
Quote: 2
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Abstract


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CLC: > Aviation, aerospace > Aerospace ( Astronauts ) > Propulsion system ( engine, propeller ) > Solid propellant rocket motor
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