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Performance Modeling of a Power Generation Gas Turbine With Wet Compression [GT2011‑46584] |
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Further Characterization of the Disturbance Field in a Transversely Excited Swirl-Stabilized Flame [GT2011‑45221] Convective and Absolute Instabilities in Reacting Bluff Body Wakes [GT2011‑45330] |
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Aero-Thermal Performance of a Cooled Winglet at Engine Representative Mach and Reynolds Numbers [GT2011‑45610] |
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Improvement on Ignition Performance for a Lean Staged Low NOx Combustor [GT2011‑46187] Suppression of NOx Emission of a Lean Staged Combustor for an Aircraft Engine [GT2011‑46256] |
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Aerothermal Investigations on Mixing Flow Field of Film Cooling With Swirling Coolant Flow [GT2011‑46838] |
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Optimal Application of Riblets on Compressor Blades and Their Contamination Behavior [GT2011‑46855] |
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A Method to Evaluate the Impact of Power Demand on HPT Blade Creep Life [GT2011‑45092] |
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Improvement on Ignition Performance for a Lean Staged Low NOx Combustor [GT2011‑46187] Suppression of NOx Emission of a Lean Staged Combustor for an Aircraft Engine [GT2011‑46256] |
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Improved Trench Film Cooling With Shaped Trench Outlets [GT2011‑45253] Predictions of Effusion Cooling With Conjugate Heat Transfer [GT2011‑45417] |
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Numerical Investigation of Low Solidity Vaned Diffuser Performance in a High-Pressure Centrifugal Compressor: Part III—Tandem Vanes [GT2011‑45382] Numerical Study on the Effects of Blade Lean on High-Pressure Centrifugal Impeller Performance [GT2011‑45383] |
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The Approach to the Development of the Next Generation Gas Turbine and History of Tohoku Electric Power Company Combined Cycle Power Plants [GT2011‑45464] |
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Experimental Study on a Notched Nozzle for Jet Noise Reduction [GT2011‑46244] |
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Experimental Study on a Notched Nozzle for Jet Noise Reduction [GT2011‑46244] |
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Experimental and Computational Approach for Jet Noise Mitigation by Mixing Control Devices [GT2011‑45200] Influence of Microjet Injection on Supersonic Jet Noise and Flow Field [GT2011‑46150] |
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Reduced Modelling for Turbine Rotor-Blade Coupled Bending Vibration Analysis [GT2011‑45776] |
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Development of Key Technologies for the Next Generation High Temperature Gas Turbine [GT2011‑45172] |
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Influence of Microjet Injection on Supersonic Jet Noise and Flow Field [GT2011‑46150] |
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Development and Strategy for A-USC Steam Turbine Cycle [GT2011‑45549] |
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Simulations of Multi-Phase Particle Deposition on a Showerhead With Staggered Film-Cooling Holes [GT2011‑45191] Effects of Surface Geometry on Film Cooling Performance at Airfoil Trailing Edge [GT2011‑45355] Heat Transfer Enhancement due to Combination of Dimples, Protrusions, and Ribs in Narrow Internal Passage of Gas Turbine Blade [GT2011‑45356] |
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Three Dimensional Design and Optimization of Transonic Rotor in Axial Flow Compressors [GT2011‑45425] |
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Innovative Starting Procedure of Siemens SGT-600 in Cold Climate Conditions [GT2011‑46409] |
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High Frequency Pressure Measurements With an Uncooled Fast Insertion Probe at Turbine Exit in a Turbojet Engine [GT2011‑45318] |
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Aerodynamic Improvement of a Transonic Fan Outlet Guide Vane Using 3D Design Optimization [GT2011‑46363] |
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Performance Analysis of a Microturbine Centrifugal Compressor From a Manufacturing Perspective [GT2011‑46374] |
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Computational Investigation of the Three-Dimensional Flow Structure and Losses in a Low Reynolds Number Microturbine [GT2011‑46587] |
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Experimental Study on a Notched Nozzle for Jet Noise Reduction [GT2011‑46244] |
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Experimental and Computational Approach for Jet Noise Mitigation by Mixing Control Devices [GT2011‑45200] Experimental and Numerical Research of Fan Bypass Duct Flows in Japanese Environmentally Compatible Engine for Small Aircraft Project [GT2011‑45481] |
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The Effect of the Operating Conditions of the Last Turbine Stage on the Performance of an Axial Exhaust Diffuser [GT2011‑45668] |
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Fuel-Forced Flame Response of a Lean-Premixed Combustor [GT2011‑46022] |
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Dynamic Simulation of Centrifugal Compressor Startup With Inlet Guide Vane [GT2011‑45810] |
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Computational and Experimental Analysis of an Industrial Gas Turbine Compressor [GT2011‑46336] |
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Impeller–Vaned Diffuser Interaction in a Centrifugal Compressor at the Best Efficiency Point [GT2011‑46223] Impeller–Vaned Diffuser Interaction in a Centrifugal Compressor at Off Design Conditions [GT2011‑46234] |
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Flowfield Measurements in a Single Row of Low Aspect Ratio Pin-Fins [GT2011‑45757] |
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Aeroelasticity at Reversed Flow Conditions: Part 1—Numerical and Experimental Investigations of a Compressor Cascade With Controlled Vibration [GT2011‑45034] |
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Analysis of Unsteadiness on Casing Treatment Mechanisms in an Axial Compressor [GT2011‑45806] |
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Surge Inception in a Transonic Centrifugal Compressor Stage [GT2011‑45116] Experimental Investigations of Corner Stall in a Linear Compressor Cascade [GT2011‑45236] A High Temperature High Bandwidth Fast Response Total Pressure Probe for Measurements in a Multistage Axial Compressor [GT2011‑45558] |
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Application of an Efficient Pressure-Temperature Coupled Solver to Industrial Hydrodynamic Bearings in Conjunction With Multi-Objective Evolutionary Optimization Technique [GT2011‑46461] |
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A Joined MBL-Zonal Method Technique for Evaluating Radiative Thermal Loads Into Combustion Chambers of Industrial Gas Turbines [GT2011‑45675] |
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Lowering Equivalence Ratio Limit for Stable Combustion in Gas Turbines by Injection of Free Radicals [GT2011‑46183] |
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Experimental and Computational Results of Distributed Combustion for Application in Current Gas Turbine Engine Combustor Architectures [GT2011‑45393] |
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Negative Stiffness in Gas Turbine Leaf Seals [GT2011‑46483] |
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Statistical and Theoretical Models of Ingestion Through Turbine Rim Seals [GT2011‑45139] Experimental Measurements of Ingestion Through Turbine Rim Seals: Part 1—Externally-Induced Ingress [GT2011‑45310] Experimental Measurements of Ingestion Through Turbine Rim Seals: Part 2—Rotationally-Induced Ingress [GT2011‑45313] Computation of Ingestion Through Gas Turbine Rim Seals [GT2011‑45314] |
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More Electric Engine Architecture for Aircraft Engine Application [GT2011‑46765] |
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More Electric Engine Architecture for Aircraft Engine Application [GT2011‑46765] |
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A Residual Stress Measurement Technique for Turbine Blade Dovetails [GT2011‑45352] |
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A Gas Turbine Engine Model of Transient Operation Across the Flight Envelope [GT2011‑45565] |