Aerodynamic and heat transfer performances of a highly loaded transonic turbine rotor with upstream generic rim seal cavity
(2021)
Journal Article
Mansouri, Z. (2021). Aerodynamic and heat transfer performances of a highly loaded transonic turbine rotor with upstream generic rim seal cavity. Propulsion and Power Research, 10(4), 317-331. https://doi.org/10.1016/j.jppr.2021.11.003
In turbine disk cavity, rim seals are fitted between the stator and its adjacent rotor disk. A coolant air injected through the turbine disk cavity to prevent the ingress of mainstream hot gases. The purpose of this paper is to investigate numericall... Read More about Aerodynamic and heat transfer performances of a highly loaded transonic turbine rotor with upstream generic rim seal cavity.