Abstract
A computer code has been applied to inviscid and viscous flows through a linear turbine cascade operating in the transonic flow regime. The Euler and Navier-Stokes equations are solved by an explicit finite-volume time-stepping procedure based on the method of Jameson et al. for the integration of the Euler equations and extended to Navier-Stokes equations by Schwamborn. The inviscid and viscous results in two-dimensions represent the profile characteristics at midspan position and the three-dimensional, viscous results include sidewall effects. A particular consideration of the flow losses gives detailed information about secondary flow behavior. The computational results are compared to experimental data for the MTU-T5.1 profile at isentropic outflow Mach numbers of 0.7, 0.9, and 1.1.
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