On the public citation graph
Blade Tip Leakage Flow and Heat Transfer with Pressure‐Side Winglet
0 signed · 73 inferred · view as graph
Inferred edges come from two machine sources: sweeps of open repository metadata (mostly SSRN and Zenodo), and a bulk OpenAlex citation snapshot. Every row below is labelled with the one it came from. Neither is a complete citation index — absence here is not evidence of absence.
Is this your work? Sign in with ORCID and put your name on the
claims that are yours.
Reference health. See whether every reference in this work resolves to a
known work and none has been retracted — and get a dated CiteStamped
badge you can embed.
What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1111/j.1749-6632.2001.tb05843.xopenalex-snapshot
A Review of Turbine Blade Tip Heat Transfer
inferredcites →https://doi.org/10.1115/1.1529190openalex-snapshot
Effects of Tip Geometry and Tip Clearance on the Mass/Heat Transfer From a Large-Scale Gas Turbine Blade
inferredcites →https://doi.org/10.1115/1.1554410openalex-snapshot
Local Mass/Heat Transfer on Turbine Blade Near-Tip Surfaces
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/10.1115/1.3227244openalex-snapshot
Rotor-Tip Leakage: Part I—Basic Methodology
inferredcites →https://doi.org/10.1115/1.3239704openalex-snapshot
Recent Progress in the Understanding of Basic Aspects of Secondary Flows in Turbine Blade Passages
inferredcites →https://doi.org/10.1115/1.3262162openalex-snapshot
Tip Leakage Flow in a Linear Turbine Cascade
inferredcites →https://doi.org/10.1115/1.3262267openalex-snapshot
The Influence of Turbine Clearance Gap Leakage on Passage Velocity and Heat Transfer Near Blade Tips: Part I—Sink Flow Effects on Blade Pressure Side
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-0195openalex-snapshot
Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade
inferredcites →https://doi.org/10.1115/2000-gt-0668openalex-snapshot
A Computational Study of a Novel Turbine Rotor Partial Shroud
inferredcites →https://doi.org/10.1115/2001-gt-0484openalex-snapshot
Aerodynamic Tip Desensitization of an Axial Turbine Rotor Using Tip Platform Extensions
inferredcites →https://doi.org/10.1115/2001-gt-0486openalex-snapshot
Methods for Desensitizing Tip Clearance Effects in Turbines
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/10.1115/99-gt-283openalex-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/gt2002-30190openalex-snapshot
Flow and Heat Transfer Predictions for a Flat-Tip Turbine Blade
inferredcites →https://doi.org/10.1615/ihtc7.1520openalex-snapshot
HEAT TRANSFER AT THE TIP OF AN UNSHROUDED TURBINE BLADE
inferredcites →https://doi.org/10.2514/6.1993-2253openalex-snapshot
Numerical and experimental investigation of turbine tip gap flow
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.4117325openalex-extracted
An Artificial Neural Network (Ann) Based Aerothermal Optimization of Film Cooling Hole Locations on the Squealer Tip of an Hp Turbine Blade
inferred← citeshttps://doi.org/10.1002/9781119910381.ch9openalex-snapshot
Passive Suppression of Rotating Stall in Mixed‐flow Pump
inferred← citeshttps://doi.org/10.1007/978-981-10-5750-2_8openalex-snapshot
Multidisciplinary Coupling Analysis and Design
inferred← citeshttps://doi.org/10.1007/s11630-009-0306-zopenalex-snapshot
Numerical investigation of active tip-clearance control through tip cooling injection in an axial turbine cascade
inferred← citeshttps://doi.org/10.1007/s12206-012-1258-xopenalex-snapshot
Tip gap flow and aerodynamic loss generation in a turbine cascade equipped with suction-side winglets
inferred← citeshttps://doi.org/10.1007/s12206-019-0119-2openalex-snapshot
Aerodynamic losses for squealer tip with different winglets
inferred← citeshttps://doi.org/10.1007/s12206-022-0626-4openalex-snapshot
Effect of blade tip pattern on blade load and vibration characteristics of a twin-stage axial flow fan
inferred← citeshttps://doi.org/10.1016/j.ast.2016.12.009openalex-snapshot
Numerical investigation of a HPT with different rotor tip configurations in terms of pressure ratio and efficiency
inferred← citeshttps://doi.org/10.1016/j.ast.2017.07.038openalex-snapshot
An evaluation of the tip clearance effects on turbine efficiency for space propulsion applications considering liquid rocket engine using turbopumps
inferred← citeshttps://doi.org/10.1016/j.ast.2022.107426openalex-snapshot
A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump
inferred← citeshttps://doi.org/10.1016/j.energy.2017.03.057openalex-snapshot
Effect of blade tip pattern on performance of a twin-stage variable-pitch axial fan
inferred← citeshttps://doi.org/10.1016/j.energy.2022.125153openalex-snapshot
An efficient winglet coverage for aeroengine turbine blade flat tip and its loss map
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2011.04.009openalex-snapshot
Experimental and numerical investigations of tip injection on tip clearance flow in an axial turbine cascade
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2023.111056openalex-snapshot
Determination of an efficient winglet for recessed tip and its loss map in aeroengine turbine cascade
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2024.107871openalex-snapshot
Enhanced cooling performance of blade tip slot cooling: Effect of slot open length
inferred← citeshttps://doi.org/10.1016/j.ijheatfluidflow.2011.11.008openalex-snapshot
Aerodynamic performance of winglets covering the tip gap inlet in a turbine cascade
inferred← citeshttps://doi.org/10.1016/j.ijheatfluidflow.2013.11.006openalex-snapshot
The effect of full coverage winglets on tip leakage aerodynamics over the plane tip in a turbine cascade
inferred← citeshttps://doi.org/10.1016/j.ijheatfluidflow.2015.07.003openalex-snapshot
Tip leakage aerodynamics over the cavity squealer tip equipped with full coverage winglets in a turbine cascade
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2015.05.023openalex-snapshot
Heat/mass transfer over the plane tip equipped with a full coverage winglet in a turbine cascade: Part 2 – Tip surface data
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2015.05.024openalex-snapshot
Heat/mass transfer over the plane tip equipped with a full coverage winglet in a turbine cascade: Part 1 – Winglet bottom surface data
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2016.03.121openalex-snapshot
Effects of squealer rim height on heat/mass transfer on the floor of cavity squealer tip in a high turning turbine blade cascade
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2016.12.026openalex-snapshot
Heat/mass transfer over the cavity squealer tip equipped with a full coverage winglet in a turbine cascade: Part 2 – Data on the cavity floor
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2016.12.027openalex-snapshot
Heat/mass transfer over the cavity squealer tip equipped with a full coverage winglet in a turbine cascade: Part 1 – Data on the winglet top surface
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2019.04.083openalex-snapshot
Chord-wise repeated thermal load change on flat tip of a turbine blade
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2022.123500openalex-snapshot
Enhancement of blade tip cooling with different position on tip cooling slot
inferred← citeshttps://doi.org/10.1016/j.oceaneng.2023.114797openalex-snapshot
Investigation on effect of anti-cavitation edge on performance and leakage vortex characteristics of tubular turbine for ocean power generation
inferred← citeshttps://doi.org/10.1017/aer.2022.6openalex-snapshot
Numerical investigations on the effect of blade tip winglet on leakage flow loss reduction for a zero inlet swirl turbine rotor
inferred← citeshttps://doi.org/10.1080/01457630903425320openalex-snapshot
Gas Turbine Blade Tip Heat Transfer and Cooling: A Literature Survey
inferred← citeshttps://doi.org/10.1080/10407782.2022.2105605openalex-snapshot
Effects of the multicavity tip coolant injection on the blade tip and the over tip casing aerothermal performance in a high-pressure turbine cascade
inferred← citeshttps://doi.org/10.1088/1742-6596/1706/1/012221openalex-snapshot
Two dimensional rotor blade numerical analysis using ANSYS
inferred← citeshttps://doi.org/10.1115/1.4034208openalex-snapshot
Heat Transfer of Winglet Tips in a Transonic Turbine Cascade
inferred← citeshttps://doi.org/10.1115/1.4045466openalex-snapshot
Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer
inferred← citeshttps://doi.org/10.1115/1.4064431openalex-snapshot
Aerothermal Optimization of Film Cooling Hole Locations on the Squealer Tip of an HP Turbine Blade
inferred← citeshttps://doi.org/10.1115/gt2018-75911openalex-snapshot
Heat Transfer Coefficient and Film Cooling Effectiveness on the Partial Cavity Tip of a Gas Turbine Blade
inferred← citeshttps://doi.org/10.1115/gt2019-90130openalex-snapshot
Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer
inferred← citeshttps://doi.org/10.1155/2009/160423openalex-snapshot
Influences of Tip Cooling Injection on Tip Clearance Control at Design and Off‐Design Incidences
inferred← citeshttps://doi.org/10.1155/2020/8841093openalex-snapshot
Influence of the Reynolds Number on Transonic Tip Flow
inferred← citeshttps://doi.org/10.1177/0957650919877057openalex-snapshot
Effect of in-service burnout on the transonic tip leakage flows over flat tip model
inferred← citeshttps://doi.org/10.1177/0957650919877276openalex-snapshot
Parametric study of injection from the casing in an axial turbine
inferred← citeshttps://doi.org/10.1177/09576509211012113openalex-snapshot
Effect of in-service burnout effect on the transonic leakage flows over cavity tip model
inferred← citeshttps://doi.org/10.1177/09576509231153304openalex-snapshot
Study on passive suppression method of rotating stall in mixed-flow pump: Using different impeller rim structures
inferred← citeshttps://doi.org/10.1179/014426011x12901840102607openalex-snapshot
Active control of tip clearance flow through casing air injection in axial turbines
inferred← citeshttps://doi.org/10.1243/09576509jpe771openalex-snapshot
Parametric study of tip cooling injection in an axial turbine cascade: Influences of injection circumferential angle
inferred← citeshttps://doi.org/10.1299/jfst.5.317openalex-snapshot
Desensitization of Tip Clearance Effects in Axial Flow Turbines
inferred← citeshttps://doi.org/10.22261/cr5jbcopenalex-snapshot
Tip gap size effects on thermal performance of cavity-winglet tips in transonic turbine cascade with endwall motion
inferred← citeshttps://doi.org/10.2322/tjsass.53.1openalex-snapshot
Control of Leakage Flow by Triple Squealer Configuration in Axial Flow Turbine
inferred← citeshttps://doi.org/10.2514/1.55134openalex-snapshot
Overtip Choking and Its Implications on Turbine Blade-Tip Aerodynamic Performance
inferred← citeshttps://doi.org/10.2514/1.t4254openalex-snapshot
Effect of Triangular Grooved Tip on Blade Tip Region Heat Transfer
inferred← citeshttps://doi.org/10.2514/1.t4541openalex-snapshot
Heat Transfer and Secondary Flow with a Multicavity Gas Turbine Blade Tip
inferred← citeshttps://doi.org/10.32604/fdmp.2022.020196openalex-snapshot
Influence of a Winglet Combined with a Groove Tip on the Performances of a Variable-Pitch Axial Flow Fan
inferred← citeshttps://doi.org/10.3390/en14237968openalex-snapshot
Effect of Mainstream Velocity on the Heat Transfer Coefficient of Gas Turbine Blade Tips
inferred← citeshttps://doi.org/10.3390/en18082099openalex-snapshot
Winglet Geometries Applied to Rotor Blades of a Hydraulic Axial Turbine Used as a Turbopump: A Parametric Analysis
inferred← citeshttps://doi.org/10.3390/en19040895openalex-snapshot
High-Pressure Turbine Aerodynamic Enhancement Using Rotor Tip Desensitization Technique
Editorial review for independent work. ICSAC — the Institute for Complexity
Science and Advanced Computing — runs a structured editorial panel for researchers
publishing outside journals, and publishes on CiteStamp rails. Submission is free
and goes through ORCID: icsacinstitute.org/submit.