Numerical study of ways to prevent side loads in an over–expanded rocket nozzles during the launch stage
IE Ivanov, IA Kryukov - Acta Astronautica, 2019 - Elsevier
The paper aims to study an issues of ensuring the safe launch of spacecraft. The
phenomenon of a turbulent boundary layer separation from the rocket engine nozzle wall …
phenomenon of a turbulent boundary layer separation from the rocket engine nozzle wall …
大扩张比喷管分离流动冷流试验研究
刘沛， 李耿， 赵利 - 实验流体力学, 2017 - syltlx.com
为研究流动分离条件下气流特性, 针对某试验大扩张比喷管, 开展了地面冷流试验研究.
试验得到了分离点前后测点压强与入口压强的变化规律, 并对测点压强数据进行了傅里叶分析 …
试验得到了分离点前后测点压强与入口压强的变化规律, 并对测点压强数据进行了傅里叶分析 …
Numerical study of ways to prevent side loads in an over–expanded rocket nozzles during the launch stage
IA Kryukov, IE Ivanov - Acta Astronautica, 2019 - elibrary.ru
The paper aims to study an issues of ensuring the safe launch of spacecraft. The
phenomenon of a turbulent boundary layer separation from the rocket engine nozzle wall …
phenomenon of a turbulent boundary layer separation from the rocket engine nozzle wall …