Evaporation and dynamic characteristics of a high-speed droplet under transcritical conditions

S Yang, Y Gao, C Deng, B Xu, F Ji… - Advances in …, 2016 - journals.sagepub.com
An evaporation and aerodynamic interaction model is developed for an isolated droplet
introduced into transcritical and strong convective environments. The new numerical model …

A review of vaporization models as design criterion for bipropellant thrust chambers

MS Gontijo - Aerospace Technic and Technology, 2022 - nti.khai.edu
In the beginning of liquid propellant rocket engine development, the thrust chamber sizes
were obtained, mainly, empirically. With the technological advancements over the years …