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Visualization of Mechanical Processes: An International Online Journal


ISSN En Línea: 2152-209X

Visualization of Mechanical Processes: An International Online Journal

DOI: 10.1615/VisMechProc.v2.i4

Tabla de Contenidos:

EXPERIMENTAL STUDY OF LOCALIZED BOUNDARY LAYER DISTURBANCES AT HIGH FREE-STREAM TURBULENCE LEVEL
Victor V. Kozlov, Mikhail M. Katasonov, Dmitry Sergeevich Sboev
DOI: 10.1615/VisMechProc.2013003838
ROUND JET IN CROSS SHEAR FLOW
Genrich R. Grek, Grigory V. Kozlov, Victor V. Kozlov, Yury A. Litvinenko, Maria V. Litvinenko
DOI: 10.1615/VisMechProc.2013005164
VERIFICATION OF CH* EMISSION IMAGING TECHNIQUE AS A MEASURE OF A FLAME'S OVERALL HEAT RELEASE RATE ON A NON-SOOTING METHANE DIFFUSION MICROFLAME
Taro Hirasawa, Kunihiro Gotanda, Yuichi Kamata, Yuji Nakamura
DOI: 10.1615/VisMechProc.2013003813
PARTICLE IMAGE VELOCIMETRY STUDY OF THE SHOCK WAVE EMANATING FROM OPEN-ENDED SHOCK TUBE
Fyodor N. Glazyrin, Irina V. Mursenkova, Irina A. Znamenskaya
DOI: 10.1615/VisMechProc.2013006876

Visualization of Mechanical Processes: An International Online Journal

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.