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Influence of Stator-Rotor Interaction on the Aerothermal Performance of Recess Blade Tips

https://doi.org/10.1115/1.4001134
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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2004.07.029openalex-snapshot
Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade
inferredcites →https://doi.org/10.1115/1.1311284openalex-snapshot
Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade
inferredcites →https://doi.org/10.1115/1.1368881openalex-snapshot
Numerical Simulation of Tip Leakage Flows in Axial Flow Turbines, With Emphasis on Flow Physics: Part I—Effect of Tip Clearance Height
inferredcites →https://doi.org/10.1115/1.1369113openalex-snapshot
Numerical Simulation of Tip Leakage Flows in Axial Flow Turbines, With Emphasis on Flow Physics: Part II—Effect of Outer Casing Relative Motion
inferredcites →https://doi.org/10.1115/1.1400114openalex-snapshot
Heat Transfer and Flow on the Blade Tip of a Gas Turbine Equipped With a Mean-Camberline Strip
inferredcites →https://doi.org/10.1115/1.1471523openalex-snapshot
Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer
inferredcites →https://doi.org/10.1115/1.1791279openalex-snapshot
Aerodynamics of Tip Leakage Flows Near Partial Squealer Rims in an Axial Flow Turbine Stage
inferredcites →https://doi.org/10.1115/1.1934410openalex-snapshot
Averaged and Time-Dependent Aerodynamics of a High Pressure Turbine Blade Tip Cavity and Stationary Shroud: Comparison of Computational and Experimental Results
inferredcites →https://doi.org/10.1115/1.2437778openalex-snapshot
Three-Dimensional Flow Prediction and Improvement of Holes Arrangement of a Film-Cooled Turbine Blade Using a Feature-Based Jet Model
inferredcites →https://doi.org/10.1115/1.2447707openalex-snapshot
Unsteady Flow Physics and Performance of a One-and-1∕2-Stage Unshrouded High Work Turbine
inferredcites →https://doi.org/10.1115/1.2775485openalex-snapshot
Flow Physics and Profiling of Recessed Blade Tips: Impact on Performance and Heat Load
inferredcites →https://doi.org/10.1115/1.2841786openalex-snapshot
Effect of Squealer Tip on Rotor Heat Transfer and Efficiency
inferredcites →https://doi.org/10.1115/1.2927985openalex-snapshot
The Development of Axial Turbine Leakage Loss for Two Profiled Tip Geometries Using Linear Cascade Data
inferredcites →https://doi.org/10.1115/1.2929188openalex-snapshot
The Effect of Blade Tip Geometry on the Tip Leakage Flow in Axial Turbine Cascades
inferredcites →https://doi.org/10.1115/1.2929189openalex-snapshot
Effects of Simulated Rotation on Tip Leakage in a Planar Cascade of Turbine Blades: Part I—Tip Gap Flow
inferredcites →https://doi.org/10.1115/1.2929190openalex-snapshot
Effects of Simulated Rotation on Tip Leakage in a Planar Cascade of Turbine Blades: Part II—Downstream Flow Field and Blade Loading
inferredcites →https://doi.org/10.1115/1.3262090openalex-snapshot
Effects of Tip Clearance on Blade Loading in a Planar Cascade of Turbine Blades
inferredcites →https://doi.org/10.1115/1.3262264openalex-snapshot
The Measurement and Formation of Tip Clearance Loss
inferredcites →https://doi.org/10.1115/1.3262266openalex-snapshot
Flow Field in the Tip Gap of a Planar Cascade of Turbine Blades
inferredcites →https://doi.org/10.1115/1.4003247openalex-snapshot
Impact of Time-Resolved Entropy Measurement on a One-and-One-Half-Stage Axial Turbine Performance
inferredcites →https://doi.org/10.1115/1.555443openalex-snapshot
Heat Transfer and Flow on the First-Stage Blade Tip of a Power Generation Gas Turbine: Part 1—Experimental Results
inferredcites →https://doi.org/10.1115/1.555444openalex-snapshot
Heat Transfer and Flow on the First-Stage Blade Tip of a Power Generation Gas Turbine: Part 2—Simulation Results
inferredcites →https://doi.org/10.1115/2000-gt-0197openalex-snapshot
Time-Averaged Heat Flux for a Recessed Tip, Lip, and Platform of a Transonic Turbine Blade
inferredcites →https://doi.org/10.1115/86-gt-245openalex-snapshot
Effects of Tip Clearance on Blade Loading in a Planar Cascade of Turbine Blades
inferredcites →https://doi.org/10.1115/91-gt-135openalex-snapshot
The Effect of Blade Tip Geometry on the Tip Leakage Flow in Axial Turbine Cascades
inferredcites →https://doi.org/10.1115/97-gt-128openalex-snapshot
Effect of Squealer Tip on Rotor Heat Transfer and Efficiency
inferredcites →https://doi.org/10.1115/99-gt-169openalex-snapshot
Heat Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas Turbine: Part 1 — Experimental Results
inferredcites →https://doi.org/10.1115/gt2006-90048openalex-snapshot
Heat-Flux Measurements and Predictions for the Blade Tip Region of a High-Pressure Turbine
inferredcites →https://doi.org/10.1115/gt2006-91073openalex-snapshot
3D Flow Prediction and Improvement of Holes Arrangement of a Film-Cooled Turbine Blade Using a Feature-Based Jet Model
inferredcites →https://doi.org/10.1115/gt2008-50807openalex-snapshot
Impact of Time-Resolved Entropy Measurement on a One-and-1/2-Stage Axial Turbine Performance
inferredcites →https://doi.org/10.21236/ad0037339openalex-snapshot
TIP CLEARANCE FLOWS IN AXIAL FLOW COMPRESSORS AND PUMPS
inferredcites →https://doi.org/10.2514/6.1996-248openalex-snapshot
A k-omega turbulence model for quasi-three-dimensional turbomachinery flows
inferredcites →https://doi.org/10.7907/mr84-wz87.openalex-snapshot
TIP CLEARANCE FLOWS IN AXIAL FLOW COMPRESSORS AND PUMPS

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

inferred← citeshttps://doi.org/10.2139/ssrn.4587567openalex-extracted
inferred← citeshttps://doi.org/10.1007/978-981-10-5750-2_8openalex-snapshot
Multidisciplinary Coupling Analysis and Design
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2016.08.173openalex-snapshot
Investigations of film cooling and heat transfer on a turbine blade squealer tip
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2018.01.090openalex-snapshot
Effect of cooling injection on the leakage flow of a turbine cascade with honeycomb tip
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2018.10.093openalex-snapshot
Influences of a multi-cavity tip on the blade tip and the over tip casing aerothermal performance in a high pressure turbine cascade
inferred← citeshttps://doi.org/10.1016/j.ast.2016.04.009openalex-snapshot
Effects of recessed blade tips on stall margin in a transonic axial compressor
inferred← citeshttps://doi.org/10.1016/j.ast.2018.11.055openalex-snapshot
Kriging surrogate model applied in the mechanism study of tip leakage flow control in turbine cascade by multiple DBD plasma actuators
inferred← citeshttps://doi.org/10.1016/j.ast.2023.108331openalex-snapshot
Refined flow organization in squealer tip gap and its impact on turbine aerodynamic performance
inferred← citeshttps://doi.org/10.1016/j.energy.2017.07.047openalex-snapshot
Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance
inferred← citeshttps://doi.org/10.1016/j.energy.2020.118170openalex-snapshot
Full aerodynamic loss data for efficient squealer tip design in an axial flow turbine
inferred← citeshttps://doi.org/10.1016/j.energy.2024.130411openalex-snapshot
Aerothermal performance of cavity tip with flow structure effects in a transonic high-pressure turbine blade
inferred← citeshttps://doi.org/10.1016/j.energy.2026.142230openalex-snapshot
Aerothermal performance analysis of turbine squealer tips with a partition rib based on tip vortex restructuring
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2022.110666openalex-snapshot
Aerodynamic performance of suction-side squealer tip in impulse/reaction turbine blade rows
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2016.07.058openalex-snapshot
Numerical investigations into the effect of squealer–winglet blade tip modifications on aerodynamic and heat transfer performance
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2017.08.090openalex-snapshot
Investigations into heat transfer and film cooling effect on a squealer-winglet blade tip
inferred← citeshttps://doi.org/10.1016/j.rineng.2023.101446openalex-snapshot
Control of the leakage flow and heat transfer characteristics at the blade tip by cavity filling
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0000919openalex-snapshot
Effective Control of Composite Honeycomb Structures on the Tip Leakage Flow in Turbine Cascade
inferred← citeshttps://doi.org/10.1080/01457632.2024.2368424openalex-snapshot
Effects of the Slotted-Cavity Tip on the Vortices and Aerothermal Performance in the High-Pressure Turbine
inferred← citeshttps://doi.org/10.1108/mmms-03-2019-0053openalex-snapshot
Numerical investigation of high pressure turbine blade tip-shaping effects on the aerothermal and dynamic performance
inferred← citeshttps://doi.org/10.1115/1.4025918openalex-snapshot
Squealer Tip Leakage Flow Characteristics in Transonic Condition
inferred← citeshttps://doi.org/10.1115/1.4047632openalex-snapshot
Investigations Into Heat Transfer and Aerodynamic Performance of a Worn Squealer Tipped Turbine Stage
inferred← citeshttps://doi.org/10.1115/1.4064273openalex-snapshot
On the Aero-Thermal Performance of Rim Film Cooling in the Squealer Tip of a Linear Turbine Cascade
inferred← citeshttps://doi.org/10.1115/1.4072050openalex-snapshot
On a Curved Cavity Floor Design Based on Heat Transfer Coefficient Distribution for a Turbine Blade Squealer Tip
inferred← citeshttps://doi.org/10.1177/0954410018801247openalex-snapshot
Effect of clearance height on tip leakage flow reduced by a honeycomb tip in a turbine cascade
inferred← citeshttps://doi.org/10.1177/0954410021998101openalex-snapshot
Investigation on the influence of the structure parameters of blade tip recess on the performance of axial flow compressor
inferred← citeshttps://doi.org/10.1177/0957650912465278openalex-snapshot
Effects of recessed blade tips on the performance and flow field in a centrifugal compressor
inferred← citeshttps://doi.org/10.1177/0957650916661459openalex-snapshot
Numerical investigations of different tip designs for shroudless turbine blades
inferred← citeshttps://doi.org/10.1177/0957650919848171openalex-snapshot
Effect of arbitrary blade tip design on tip leakage flow
inferred← citeshttps://doi.org/10.21595/jve.2015.15753openalex-snapshot
Effects of stator-rotor interaction on unsteady aerodynamic load of compressor rotor blades
inferred← citeshttps://doi.org/10.2322/tjsass.64.293openalex-snapshot
Effect of Cutbacks on Tip Leakage Flow and Film-Cooling Effectiveness of a Turbine Blade Tip under Relative Moving Condition
inferred← citeshttps://doi.org/10.33737/gpps21-tc-175openalex-snapshot
Effects of Squealer Width and Height on Aerodynamic Performance of Tip-Leakage Flow of Cavity Tips
inferred← citeshttps://doi.org/10.3389/fenrg.2022.845350openalex-snapshot
Effect of Film Position on the Flow and Heat Transfer Characteristics of Full-Ribbed Rotor Tip
inferred← citeshttps://doi.org/10.3389/fenrg.2022.994811openalex-snapshot
Influence of grooved rib tip structure on tip loss and heat transfer in a gas turbine blade
inferred← citeshttps://doi.org/10.3390/pr14152422openalex-snapshot
Investigation of the Aero-Thermal Performance of a Turbine Blade Tip with Trapezoidal Slots and Rib Slots in Transonic Flow
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