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Visualization of Mechanical Processes: An International Online Journal


ISSN Онлайн: 2152-209X

Visualization of Mechanical Processes: An International Online Journal

DOI: 10.1615/VisMechProc.v3.i1

Содержание:

Digital holographic interferometry at F4-ONERA hypersonic wind tunnel
Jean-Michel Desse, Jacques Soutade, Paul Viguier, Pascal Picart, Marc Ferrier, Laurent Serre
DOI: 10.1615/VisMechProc.2013007554
INSTABILITY OF A SWEPT-WING BOUNDARY LAYER MODULATED BY STATIONARY FLOW PERTURBATIONS
Valery G. Chernoray, Alexander V. Dovgal, Genrich R. Grek, Victor V. Kozlov, Yury A. Litvinenko, Lennart Lofdahl
DOI: 10.1615/VisMechProc.2013006967
SHEAR SENSITIVE LIQUID CRYSTALS FOR DIAGNOSTICS OF BOUNDARY LAYER STRUCTURE IN AERODYNAMICAL EXPERIMENT
Galina Zharkova, Valentina Kovrizhina, Alexander Petrov
DOI: 10.1615/VisMechProc.2014007940
EVOLUTION OF NONLINEAR PANEL FLUTTER OSCILLATIONS
Anastasia Shishaeva, Vasily Vladimirovich Vedeneev
DOI: 10.1615/VisMechProc.2014011122
VISUALIZATION OF A SUBSONIC JET WITH ACOUSTIC EXCITATION
Tatiana M. Makarenko
DOI: 10.1615/VisMechProc.2014007107

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.