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ISSN 在线: 2152-209X

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DOI: 10.1615/VisMechProc.v3.i3

内容列表:

EXPERIMENTAL AND THEORETICAL RESEARCHES ON INFLUENCE OF PARAMETRIC EXCITATION ON THE FLUTTER CRITICAL SPEED OF AIRCRAFT MODEL OF WING
Andrei Yur'evich Mazutskii, Artem Ribhatovich Zagidulin, Maxim Mihailovich Druzhinin
DOI: 10.1615/.2016014025
SIMULATION OF DROPS MOTION IN CHANNELS USING FAST MULTIPOLE METHOD /GRAPHICS PROCESSORS ACCELERATED BOUNDARY ELEMENT METHOD
Olga A. Abramova, Yulia A. Pityuk, Nail A. Gumerov, Iskander S. Akhatov
DOI: 10.1615/.2016016720

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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.