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ssrn.3967945

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What this work says

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

inferredcites →https://doi.org/10.1016/0894-1777(94)90118-xopenalex-extracted

Experimental methods for engineers

inferredcites →https://doi.org/10.1016/c2009-0-64242-2openalex-extracted

Gas Turbine Engineering Handbook

inferredcites →https://doi.org/10.1016/j.applthermaleng.2017.07.188openalex-extracted

Improvement on film cooling effectiveness by a combined slot-effusion scheme

inferredcites →https://doi.org/10.1016/j.applthermaleng.2017.08.165openalex-extracted

Heat transfer of impinging jet arrays onto half-smooth, half-rough target surfaces

inferredcites →https://doi.org/10.1016/j.applthermaleng.2018.11.116openalex-extracted

Experimental and numerical investigations of overall cooling effectiveness on a vane endwall with jet impingement and film cooling

inferredcites →https://doi.org/10.1016/j.applthermaleng.2021.117439openalex-extracted

Influence of Biot number and geometric parameters on the overall cooling effectiveness of double wall structure with pins

inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2018.07.085openalex-extracted

Study on analogy principle of overall cooling effectiveness for composite cooling structures with impingement and effusion

inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2018.12.080openalex-extracted

Enhanced film cooling performance of a row of cylindrical holes embedded in the saw tooth slot

inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2020.119449openalex-extracted

Effects of impingement gap and hole arrangement on overall cooling effectiveness for impingement/effusion cooling

inferredcites →https://doi.org/10.1115/1.3140282openalex-extracted

Enhancement of Impingement Cooling in a High Cross Flow Channel Using Shaped Impingement Cooling Holes

inferredcites →https://doi.org/10.1115/1.3213555openalex-extracted

Adiabatic and Overall Effectiveness Measurements of an Effusion Cooling Array for Turbine Endwall Application

inferredcites →https://doi.org/10.1115/1.4006872openalex-extracted

Overall Effectiveness for a Film Cooled Turbine Blade Leading Edge With Varying Hole Pitch

inferredcites →https://doi.org/10.1115/1.4023105openalex-extracted

Overall and Adiabatic Effectiveness Values on a Scaled Up, Simulated Gas Turbine Vane

inferredcites →https://doi.org/10.1115/1.4024681openalex-extracted

Sensitivity of the Overall Effectiveness to Film Cooling and Internal Cooling on a Turbine Vane Suction Side

inferredcites →https://doi.org/10.1115/1.4025835openalex-extracted

Overall Effectiveness of a Blade Endwall With Jet Impingement and Film Cooling

inferredcites →https://doi.org/10.1115/1.4036200openalex-extracted

Experimentally Measured Effects of Incidence Angle on the Adiabatic and Overall Effectiveness of a Fully Cooled Turbine Airfoil With Shaped Showerhead Holes

inferredcites →https://doi.org/10.1115/1.4036361openalex-extracted

Experimental Investigation of Endwall Heat Transfer With Film and Impingement Cooling

inferredcites →https://doi.org/10.1115/1.4041645openalex-extracted

Experimental Evaluations of the Relative Contributions to Overall Effectiveness in Turbine Blade Leading Edge Cooling

inferredcites →https://doi.org/10.1115/gt2012-69110openalex-extracted

Sensitivity of the Overall Effectiveness to Film Cooling and Internal Cooling on a Turbine Vane Suction Side

inferredcites →https://doi.org/10.1115/gt2017-63421openalex-extracted

Overall Cooling Effectiveness Measurements on Pressure Side Surface of the Nozzle Guide Vane With Optimized Film Cooling Hole Arrangements

inferredcites →https://doi.org/10.1115/gt2018-75334openalex-extracted

Experimental Evaluations of the Relative Contributions to Overall Effectiveness in Turbine Blade Leading Edge Cooling

What points at this work

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

inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2025.110236openalex-snapshot

Study on the influence of combustor outlet temperature distortion on turbine aerodynamic heat transfer

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