摘要
凝聚相微粒尺寸分布对固体火箭发动机燃烧室效率和喷管效率有影响。本文介绍了引起固体火箭发动机两相流动损失的凝聚相微粒尺寸分布。
The condensed phase particle size distribution affects the combustion chamber and nozzle efficiency of solid rocket motors to some extent.The paper introduces the measurement method research status and the condensed phase particle size distribution leading to the two phase flow loss for solid rocket motor.
出处
《固体火箭技术》
EI
CAS
CSCD
2000年第3期25-28,共4页
Journal of Solid Rocket Technology
