EFFECTS OF VARYING TIP CLEARANCE AND AXIAL GAP ON AXIAL-FLOW TURBINE STAGE PERFORMANCE ( PRESENT STATE OF THE ART)

Computed Effect of Varying Tip Clearance and Axial Gap on Gas Turbine Stage Performance Part (I): (Steady Flow)

EXPERIMENTAL AND NUMERICAL INVESTIGATION OF THE FLOW THROUGH CASCADES

EFFECT OF AXIAL GAP ON THE AERODYNAMICS OF 1 AND 1.5 STAGE TURBINES

A Numerical Study of the Effect of Endwall Injection Blowing Ratio on a High Pressure Turbine Cascade Performance

A Numerical Study of the Effect of Endwall Injection Inclination Angle on a High Pressure Turbine Cascade Performance

AERODYNAMIC PERFORMANCE AND ASSOCIATED NOISE GENERATION SPECTRA OF AIRFOIL

Effect of Changing Maximum Camber Position of the Turbine Blade on its Aerodynamic Performance

ON LOSS MECHANISM THROUGH REACTION TURBINE CASCADE: EFFECT OF SPACE-CHORD RATIO

EXPERIMENTAL INVESTIGATION OF THE WAKE BEHIND A CASCADE OF AIRFOILS AND ISOLATED AIRFOIL