Analysis of conjugate heat transfer of a gas turbine first stage nozzle

Adiabatic and conjugate cooling effectiveness analysis of a new hybrid scheme

“…Therefore redesign and relocation of the film hole shapes in these regions were proposed to protect these areas. Mazur et al [19] analyzed the conjugate heat transfer for the first stage airfoil nozzle (vane) by investigating thermal load and temperature distribution around the nozzle in order to estimate the van life including the step change in material properties.…”

Transient heat transfer between a turbulent lean partially premixed flame in limit cycle oscillation and the walls of a can type combustor

“…Considering that turbine nozzles and blades are exposed to the maximum and limiting temperature of a cycle, in recent years several researches have been conducted in order to investigate the heat transfer of gas turbine blades by conducting either steady state or transient Conjugate Heat Transfer calculations (CHT) [9,10]. It will however have to be recognized that the gas turbine combustor locally is exposed to the highest temperatures in the engine.…”

Coupled simulation of heat transfer and temperature of the composite rocket nozzle wall

“…Z. Mazur et al analyzed the conjugate heat transfer of a gas turbine first stage nozzle [11]. John quantity of the black body r radiative t throat W. Edwards discussed the problems of heat transfer in ASRM nozzle design and development [8].…”