| 61 |
Kim, J. S., Kim, K. H., & Lee, J. (2023). Improvement of Heat Transfer Model Considering Heat Transfer Deterioration of Supercritical Fluid in Cooling Channel of Scramjet Propulsion System. International Journal of Aeronautical and Space Sciences, 1-13.
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| 60 |
Seo, J., Kim, J. S., & Kim, K. H. (2023). Improved prediction of the thermodynamic properties of JP-10 using an extended Redlich-Kwong-Peng-Robinson equation of state. Journal of Industrial and Engineering Chemistry, 123, 88-103.
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| 59 |
Seo, S. H., Ji, W. G., Jeong, J., & Kim, K. H. (2023). Wind tunnel experiment and thermodynamic modeling for dry-snow accretion on a heated surface. International Journal of Heat and Mass Transfer, 207, 123990.
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| 58 |
Rhee, J., Oh, J., Kung, T., & Kim, K. (2023). An Implicit Multicloud Convergence Accelerator for Compressible Flows. International Journal of Aeronautical and Space Sciences, 1-11.
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| 57 |
Choi, J. Y., Unnikrishnan, U., Hwang, W. S., Jeong, S. M., Han, S. H., Kim, K. H., & Yang, V. (2022). Effect of fuel temperature on flame characteristics of supersonic turbulent combustion. Fuel, 329, 125310.
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| 56 |
Kim, P., Choi, W., & Kim, K. H. (2022). Analysis of Aerodynamic Characteristics of Rear Wing Mounted on Fastback Type Vehicle. International Journal of Automotive Technology, 23(5), 1255-1268.
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| 55 |
Kim, J. S., Seo, J., Han, D., & Kim, K. H. (2022). Prediction of thermochemical and transport properties of hydrocarbon aviation fuel in supercritical state with thermal decomposition. Fuel, 325, 124805.
|
| 54 |
Lee, J. W., & Kim, K. H. (2023). Pressure Characteristics Exerted on Base by Underexpanded Jet of Powered-On Supersonic Vehicles. Journal of Spacecraft and Rockets, 60(1), 4-21.
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| 53 |
Baek, J., Choi, D., & Kim, K. H. (2022). Numerical Investigation of Diffusers in Arc-Heated Wind Tunnel: Introducing a Novel and Efficient Hypersonic Diffuser. Journal of Aerospace Engineering, 35(5), 04022070.
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| 52 |
Han, D., Kim, J. S., & Kim, K. H. (2022). Conjugate thermal analysis of X-51A-like aircraft with regenerative cooling channels. Aerospace Science and Technology, 126, 107614.
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