Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations †
Schneider, M.; Schiffer, H.-P.; Lehmann, K. Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations. Int. J. Turbomach. Propuls. Power 2017, 2, 20. https://doi.org/10.3390/ijtpp2040020
Schneider M, Schiffer H-P, Lehmann K. Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations. International Journal of Turbomachinery, Propulsion and Power. 2017; 2(4):20. https://doi.org/10.3390/ijtpp2040020
Chicago/Turabian StyleSchneider, Marius, Heinz-Peter Schiffer, and Knut Lehmann. 2017. "Parameterised Model of 2D Combustor Exit Flow Conditions for High-Pressure Turbine Simulations" International Journal of Turbomachinery, Propulsion and Power 2, no. 4: 20. https://doi.org/10.3390/ijtpp2040020