Visualization of Mechanical Processes: An International Online Journal

DOI: 10.1615/VisMechProc.v3.i1

Table of Contents:

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 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

Experimental facility for the visualization of vortex rings in a subsonic 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)

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.