Numerical modeling of hot gas ingestion into the rotor-stator disk cavities of a subscale 1.5-stage axial gas turbine - Concepedia

Concepedia

Publication | Closed Access

Numerical modeling of hot gas ingestion into the rotor-stator disk cavities of a subscale 1.5-stage axial gas turbine

15

Citations

33

References

2018

Year

Masoud Ghasemian, Marko Princevac, Yong W. Kim, Hans D. Hamm

International Journal of Heat and Mass Transfer

Hot Gas IngestionRotor-stator Disk CavitiesGas Turbine CombustionHeat TransferGas Turbine EngineNumerical ModelingFluid Machinery

References

	Year	Citations

Page 1