Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Seong-Mok Moon"'
Autor:
Kyoung-Hoon Lee, Seong-Mok Moon
Publikováno v:
Transaction of the Korean Society of Automotive Engineers. 28:771-780
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f0665f7315ba3c91c19424c0f71eabf
https://doi.org/10.7467/ksae.2020.28.11.771
https://doi.org/10.7467/ksae.2020.28.11.771
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 19:55-64
In this study, a 3-D flame cooling analysis is conducted to examine thermal safety for the flame deflector of the 75 tonf class propulsion test facility, and the safe discharge of the exhaust gas is assessed by using numerical results. The Mixture mu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5964ea2924c41f067e715fc1ce247280
https://doi.org/10.6108/kspe.2015.19.2.055
https://doi.org/10.6108/kspe.2015.19.2.055
Publikováno v:
Journal of Fluid Machinery. 15:25-31
A computational study on the improvement of the pressure loss of intake system, which is located at engine manifold of the combat vehicle, has been conducted using a finite-volume-based, Reynolds-Averaged Navier-Stokes (RANS) solver. The computationa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::139b1856baced0489878a95410c4c28f
https://doi.org/10.5293/kfma.2012.15.3.025
https://doi.org/10.5293/kfma.2012.15.3.025
Parametric Study on the Mixing Enhancement of Parallel Supersonic-subsonic Wakes Using Wall Cavities
Publikováno v:
Numerical Heat Transfer, Part A: Applications. 54:367-389
A series of computational studies on the enhancement of parallel supersonic-subsonic mixing wakes, where M 1 = 1.78 and M 2 = 0.30 at baseline, is conducted and compared with available experimental data. The mixing problem of this parallel flow is ch
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::33eb53de3f9ae406b3f16123e162b632
https://doi.org/10.1080/10407780802164629
https://doi.org/10.1080/10407780802164629
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 32:20-28
For the prediction on the onset of oblique shock wave-induced vortex breakdown, computational studies on the Oblique Shock wave/Vortex Interaction (OSVI) are conducted and compared with both experimental results and analytic mode1. A Shock-stable num
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::667c781df73c2e7f494ada3221061148
https://doi.org/10.5139/jksas.2004.32.8.020
https://doi.org/10.5139/jksas.2004.32.8.020