AERO-THERMAL INVESTIGATION OF A HIGHLY LOADED TRANSONIC LINEAR TURBINE GUIDE VANE CASCADE : A test case for inviscid and viscous flow computations
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American Society of Mechanical Engineers |
7
テクニカルペーパー
Computational Investigation of Hypersonic Viscous/Inviscid Interactions in High Enthalpy Flows
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
3
テクニカルペーパー
Investigation of the flow field downstream of a turbine trailing edge cooled nozzle guide vane
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
National Aeronautics and Space Administration |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |