Highly Loaded Multi-stage Fan Drive Turbine-leaned Stator Configuration Design |
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aerodynamic design air turbine testing Angle Inlet axial station Axial Velocity Blade Force Blade Inlet Angles blade loading Blade Pitch computer program degree tangentially leaned Design Inlet Angle Effect of Stage Estimated Vibratory Capabilities fan drive turbine Figure 17 fluid gas bending Hi-c high stage loading high-lift devices high-lift turbine key detail drawings lean and axial lean and sweep leaned stage three Mechanical Design Flowpath Midcv moment of inertia Multistage Fan Drive NASA Normalized Axial Width Number of Vanes plain blade turbine radial radial-equilibrium equation Radius rotor hub Stage Three Blade stage three stator Stage Three Vane static pressure gradient stator hub stator lean STEADY-STATE MECHANICAL STRESSES Steady-state stresses tandem blade tangentially leaned stage tangentially leaned stator Tangentially Leaned Vane Three Blade Inlet Three Vane Lean Tip Shroud Turbine Aerodynamic Flowpath turbine rig turbofan Unguided Turning Vane Axial Sweep VANE DESIGN DATA Vane Exit vane section Vector Diagram Study