Computational Study of clocking an Embedded Stage in a 4-Stage Industrial Turbine.
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Effects of Blade Count on Hot Streak Clocking Simulations using Linearized and Nonlinear Methods
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Effects of Endwall Geometry and Stacking on Two-Stage Supersonic Turbine Performance.
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Experimental and numerical investigation of airfoil clocking and inter-blade-row gap effects on axial compressor performance
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Full-annulus simulations of airfoil clocking in a compressor at off-design operating conditions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Study of the effects of hot streaks on heat transfer in subsonic and transonic flows
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |