A Navier-Stokes analysis of film cooling in a turbine blade
- 11 January 1993
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Aerodynamic and heat transfer analysis of the low aspect ratio turbine using a 3D Navier-Stokes codePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling for Turbine Blade ApplicationsJournal of Turbomachinery, 1990
- Prediction of Film Cooling by a Row of Holes With a Two-Dimensional Boundary-Layer ProcedureJournal of Turbomachinery, 1987
- Unsteady Aerodynamic and Heat Transfer Processes in a Transonic Turbine StageJournal of Engineering for Gas Turbines and Power, 1985
- A flexible grid embedding technique with application to the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983