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ISSN 在线: 2152-209X

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DOI: 10.1615/VisMechProc.v1.i3

SPECIAL ISSUE OF ASV11 - Part 1


内容列表:

INTRODUCTION TO SPECIAL ISSUE OF ASV11 - Part 1
Nobuyuki Fujisawa
DOI: 10.1615/VisMechProc.v1.i3.10
OH-PLIF MEASUREMENT OF EDGE-FLAME ESTABLISHED IN COUNTERFLOW FIELD
W. Nishiwaki, H. Mochizuki, T. Kouchi, Kenichi Takita
DOI: 10.1615/VisMechProc.v1.i3.20
EXPERIMENTAL AND THEORETICAL STUDY ON FLOOD BORE PROPAGATION AND MUSHROOM JET GENERATION OF DAM-BREAK FLOW
H. H. Hwung, Ray Yang, Y. C. Tie, W.Y. Hsu, P. C. Kuo, Igor V. Shugan
DOI: 10.1615/VisMechProc.v1.i3.30
VISUALIZATION OF THREE-DIMENSIONAL STRUCTURE OF MIXED CONVECTION IN A RECTANGULAR CHANNEL WITH A CAVITY
Yuichi Funawatashi, Hironobu Watanabe, Tetsuya Mizukami
DOI: 10.1615/VisMechProc.v1.i3.40
VISUALIZATION OF PROCESSES CAUSED BY DIRECT CURRENT PLASMA DISCHARGE IN HYPERSONIC FLOW OVER FLAT PLATE
Yasumasa Watanabe, Kojiro Suzuki
DOI: 10.1615/VisMechProc.v1.i3.50
OIL AND SMOKE FLOW VISUALIZATION PAST TWO-DIMENSIONAL AIRFOILS FOR AN UNMANNED AERIAL VEHICLE
LUIS VELAZQUEZ-ARAQUE, Jiri Nozicka
DOI: 10.1615/VisMechProc.v1.i3.60

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An International Online Journal Visualization of Mechanical Processes for iPad An International Online Journal Visualization of Mechanical Processes for iPad
Experimental facility for the visualization of vortex rings in a subsonic jet. Experimental facility for the visualization of vortex rings in a subsonic jet.
Movies demonstrating the development of vortex rings in a jet Movies demonstrating the development of vortex rings in a jet
The excitation of the vortex ring oscillations at the pulse interaction with a rigid obstacle (streamlining of a thin cylinder of 0.3 cm diameter) The excitation of the vortex ring oscillations at the pulse interaction with a rigid obstacle (streamlining of a thin cylinder of 0.3 cm diameter)
Drawing (a), and photographic image (b) of Specimen T60030N. Drawing (a), and photographic image (b) of Specimen T60030N.
Model photography in the wind tunnel: wind tunnel UT-1 (TsAGI) operated in Ludwig scheme, test duration 40 msec, two-color TSP. Model photography in the wind tunnel: wind tunnel UT-1 (TsAGI) operated in Ludwig scheme, test duration 40 msec, two-color TSP.