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ISSN 在线: 2152-209X

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DOI: 10.1615/VisMechProc.v2.i3

内容列表:

EXPERIMENTAL INVESTIGATION OF FLUID FLOW IN A HORIZONTAL ENCLOSURE WITH BAFFLE PLATES ON TWO OPPOSITE WALLS
P. K. Bose, Dipak Sen, Rajsekhar Panua, Ajoy Kumar Das
DOI: 10.1615/VisMechProc.2013004763
FLOW VISUALIZATION AND PRESSURE DISTRIBUTION ON THE WALLS OF TRANSVERSE CAVITY AT A CHANGE IN TILT ANGLE OF THE FRONT AND BACK WALLS
A. Yu. D'yachenko, Viktor I. Terekhov, Nadezhda I. Yarygina
DOI: 10.1615/VisMechProc.v2.i1.20
VORTICAL STRUCTURE DYNAMICS OF SEPARATED CHANNEL FLOW BEHIND A SEMICYLINDRICAL RIB AT LATE STAGES OF LAMINAR-TURBULENT TRANSITION
Valery M. Molochnikov, Olga A. Dushina, Anton A. Paereliy
DOI: 10.1615/VisMechProc.v2.i1.30
INFLUENCE OF INITIAL CONDITIONS AT THE NOZZLE EXIT AND ACOUSTICAL ACTION ON THE STRUCTURE AND STABILITY OF A PLANE JET
Victor V. Kozlov, Genrich R. Grek, Yury A. Litvinenko, Grigory V. Kozlov, Maria V. Litvinenko
DOI: 10.1615/VisMechProc.2013005162
ORTHOGONALLY STIFFENED SHELL VIBRATIONS UNDER POINT IMPULSE
Leonid Anatolievich Lazarev
DOI: 10.1615/VisMechProc.2013004981

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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.