Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 1 of 1 for “"Aerodynamic Loss, Heat Transfer, Mach Number, Reynolds Numbers, Transition, Vane Cascade"”.

  1. Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows

    … the low pressure turbine experiences low Reynolds number flow, which produces a laminar boundary layer on airfoil surfaces. The integrity of the laminar boundary layer is highly susceptible to flow disturbances resulting from blade wakes and freestream turbulence. This susceptibility often …

    nodak Repository record for Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows (opens in a new tab)