Aerodynamic and heat transfer analysis of the low aspect ratio turbine using a 3D Navier-Stokes code
- 24 June 1991
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Stagnation Point and Surface Heat Transfer for a Turbine Stage: Prediction and Comparison With DataJournal of Turbomachinery, 1989
- Tip Leakage Flow in a Linear Turbine CascadeJournal of Turbomachinery, 1988