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Young Jun Kang

Korea Aerospace University

Department of Business Administration

200-1, Hwajeon-dong, Deokyang-gu

Goyang-city, 421-791

Korea, Republic of (South Korea)

  • Korea Aerospace University

SCHOLARLY PAPERS

6

DOWNLOADS

262

TOTAL CITATIONS

2

Scholarly Papers (6)

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1.

Effect of an Inlet Keyhole Slot Geometry on Crossflow-Fed-Film Cooling Hole

Number of pages: 29 Posted: 17 Oct 2024
Won Seok Lim, Young Jun Kang, Suhyeon Park and Jae Su Kwak
Korea Aerospace University, Korea Aerospace University, Korea Aerospace University and Korea Aerospace University
Downloads 51 (1,063,489)

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Crossflow, Film cooling, Gas turbine, Heat transfer, Pressure sensitive paint technique

2.

Heat Transfer Augmentation in a Stationary 1:1 Square Channel with Round Shaped Ribs

Number of pages: 19 Posted: 09 Oct 2023
Young Jun Kang, Jin Young Jeong, Gi Mun Kim, Hyeok Je Kim and Jae Su Kwak
Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University and Korea Aerospace University
Downloads 50 (1,121,190)

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Gas turbine, heat transfer, internal cooling, ribbed channel, round rib, transient liquid crystal technique

3.

Heat Transfer Coefficient in Rotating Channels with Round Rib Turbulators

Number of pages: 19 Posted: 12 Feb 2025
Jongsu Oh, Young Jun Kang, Woojun Kim and Jae Su Kwak
Korea Aerospace University, Korea Aerospace University, Korea Aerospace University and Korea Aerospace University
Downloads 48 (1,109,210)
Citation 1

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gas turbine, Rotating Channel, Heat transfer, Rib Turbulators, Thermochromic liquid crystals

4.

Effect of Relative Location of Film Cooling Hole with Internal Angled Ribs on the Film Cooling Effectiveness of a Gas Turbine Blade

Downloads 41 (1,196,171)

Effect of Relative Location of Film Cooling Hole with Internal Angled Ribs on the Film Cooling Effectiveness of a Gas Turbine Blade

Number of pages: 23 Posted: 29 Aug 2025
Young Jun Kang, Jin Young Jeong, Hyeok Je Kim, Gi Mun Kim, Chan Gyu Lee and Jae Su Kwak
Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University and Korea Aerospace University
Downloads 29 (1,385,838)

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Gas turbine, Film cooling, Internal channel, Location of film cooling hole

Effect of Relative Location of Film Cooling Hole with Internal Angled Ribs on the Film Cooling Effectiveness of a Gas Turbine Blade

Number of pages: 23 Posted: 28 Aug 2025
Young Jun Kang, Jin Young Jeong, Hyeok Je Kim, Gi Mun Kim, Chan Gyu Lee and Jae Su Kwak
Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University and Korea Aerospace University
Downloads 12 (1,598,105)

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Gas turbine, Film cooling, Internal channel, Location of film cooling hole

5.

Experimental Optimization of Butterfly-Shaped Film Cooling Hole Configuration with a 30 Degree Injection Angle

Number of pages: 32 Posted: 19 Sep 2023
Jin Young Jeong, Ye Rim Jo, Gi Mun Kim, Young Jun Kang, Min Seok Kang and Jae Su Kwak
Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University and Korea Aerospace University
Downloads 37 (1,236,159)
Citation 1

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Gas turbine, Heat transfer, Advanced Film cooling, Optimization

6.

Heat Transfer Measurements on a Flat Plate and Cylinders at High Velocity Conditions: Comparison of Calculation Models with Infrared Thermography

Number of pages: 16 Posted: 14 Nov 2023
Jae Su Kwak, Woojun Kim, Jin Young Jeong, Young Jun Kang, Hyeok Je Kim, Gi Mun Kim and Suhyeon Park
Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University, Korea Aerospace University and Korea Aerospace University
Downloads 35 (1,249,711)

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heat transfer coefficient, one-dimensional semi-infinite solid assumption, Adiabatic wall temperature, Transient, Linear regression