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Jun LI

affiliation not provided to SSRN

SCHOLARLY PAPERS

7

DOWNLOADS

206

TOTAL CITATIONS

2

Scholarly Papers (7)

1.

Overall Cooling Effectiveness of Blade Leading Edge with Double Swirl Chamber: Effect of Turbulence Intensity and Wall Thickness

Number of pages: 24 Posted: 26 Sep 2023
affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and affiliation not provided to SSRN
Downloads 50 (1,063,489)

Abstract:

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Gas turbine, Biot number, Turbulence intensity, Wall thickness, Cross flow, Overall cooling effectiveness

2.

Effect of Film Hole Diameter and Attack Angle on the Film Cooling Performance of Leading Edge with Double Swirl Chamber Under Crossflow Condition

Number of pages: 31 Posted: 03 Oct 2023
affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and affiliation not provided to SSRN
Downloads 37 (1,222,651)
Citation 2

Abstract:

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Gas turbine, Leading edge, Crossflow intensity, Film cooling diameter, Attack angle

3.

Efficient Uncertainty Quantification on the Aerodynamic Performance of the Transonic Multi-Cavity Squealer Tip

Number of pages: 38 Posted: 13 Oct 2022
affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and affiliation not provided to SSRN
Downloads 32 (1,290,922)

Abstract:

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uncertainty quantification, aerothermal performance, Turbine blade, Multi-cavity Squealer Tip, sensitivity analysis

4.

Effect of Crossflow in Double Swirl Chamber on the Film Cooling Effectiveness of Leading Edge

Number of pages: 37 Posted: 08 May 2023
affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and affiliation not provided to SSRN
Downloads 29 (1,332,057)

Abstract:

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Gas turbine, Leading edge, Double swirl chamber, Film cooling, Crossflow intensity

5.

Influence of Blowing Ratio and Film Hole Position on the Film Cooling Effectiveness of Double Swirl Cooling with Film Holes

Number of pages: 32 Posted: 17 Dec 2022
affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and affiliation not provided to SSRN
Downloads 26 (1,372,601)

Abstract:

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Gas Turbine, Turbine Blade;Leading Edge, Double swirl cooling, Film Cooling

6.

Large Eddy Simulation on Unsteady Flow and Heat Transfer Behaviors of Double Swirl Cooling Configuration

Number of pages: 31 Posted: 03 May 2024
affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN and affiliation not provided to SSRN
Downloads 22 (1,424,331)

Abstract:

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Gas turbine, Leading edge, Double swirl cooling, Large eddy simulation

7.

Endwall Flow Pulsation Patterns and Aerothermal Performance of Hydrogen-combustion Turbines

Number of pages: 27 Posted: 16 Apr 2026
affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, affiliation not provided to SSRN, Virginia Polytechnic Institute and State University and Virginia Polytechnic Institute and State University
Downloads 10 (1,548,648)

Abstract:

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Hydrogen-combustion turbines, Turbine endwall, Unsteady aerothermal performance, Flow pulsation patterns, Transient response characteristics