Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Seung-Kyu Hong"'
Publikováno v:
SoftwareX, Vol 28, Iss , Pp 101922- (2024)
The presentation video is an effective way to convey information, but it has the disadvantage of requiring a lot of time and effort to consume, as one needs to grasp both the visual and auditory information in the video to understand it. In this stud
Externí odkaz:
https://doaj.org/article/0d2d42c6e0944872bcb41c20511c9ea6
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 33:1-8
For study on the unsteady wall interference effect, flows around a circular cylinder in closed test-section wind tunnels have been numerically investigated by solving compressible Navier-Stokes equations. The numerical scheme is based on a node-based
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f2a870d2af3cd7189bc7d7b02b39ca9a
https://doi.org/10.5139/jksas.2005.33.7.001
https://doi.org/10.5139/jksas.2005.33.7.001
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
Publikováno v:
Journal of Spacecraft and Rockets. 41:735-744
The jet impinging flow structure exhibits such complex natures as shock shell, plate shock, and Mach disk, depending on the flow parameters. The main parameters are the ratio of the jet pressure to the ambient pressure and the distance between the no
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::14a90022f30fc69ad5fc49af12c08ac3
https://doi.org/10.2514/1.13077
https://doi.org/10.2514/1.13077
Publikováno v:
Journal of Computational Physics. 185:342-374
This paper deals with the development of an improved Roe scheme that is free from the shock instability and still preserves the accuracy and efficiency of the original Roe's Flux Difference Splitting (FDS). Roe's FDS is known to possess good accuracy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::934e1364c33a151f3a005ee51e482c61
https://doi.org/10.1016/s0021-9991(02)00037-2
https://doi.org/10.1016/s0021-9991(02)00037-2
Autor:
Kwang-Seop Lee, Seung-Kyu Hong
Publikováno v:
International Journal of Aeronautical and Space Sciences. 3:67-75
In the course of missile system design, jet plume impingement is encountered in designing airframe as well as launchers, requiring careful investigation of its effect on the system. In the present paper, recent works on such topic are presented to de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54ddc219e6fcb4e93120c13ffb793507
https://doi.org/10.5139/ijass.2002.3.2.067
https://doi.org/10.5139/ijass.2002.3.2.067
Publikováno v:
40th AIAA Aerospace Sciences Meeting & Exhibit.
This paper deals with the development of an improved Roe scheme that is free from the shock instability and still preserves the accuracy and efficiency of the original Roe's Flux Difference Splitting (EDS). Roe's FDS is known to possess good accuracy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fab171a4cf828fec1b8f4e686d261f6b
https://doi.org/10.2514/6.2002-548
https://doi.org/10.2514/6.2002-548
Publikováno v:
Managing Intellectual Property. Jun99, Issue 90, p51. 2p.