Crossflow vortex and transition measurements by use of multielement hot films

This publication has 12 references indexed in Scilit:

• A transition detection study at Mach 1.5, 2.0 and 2.5 using a micro-thin hot-film system
  Published by Institute of Electrical and Electronics Engineers (IEEE) ,2003
• Measurement of crossflow vortices, attachment-line flow, and transition using microthin hot films
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1990
• Stability of Three-Dimensional Boundary Layers
  Annual Review of Fluid Mechanics, 1989
• A unique measurement technique to study laminar-separation bubble characteristics on an airfoil
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1987
• Three-dimensional transition studies at ONERA/CERT
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1987
• Experimental study of instability modes in a three-dimensional boundary layer
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1987
• Some expectation on the mechanism of cross-flow instability in a swept wing flow
  Acta Mechanica, 1987
• Experiments on the stability of crossflow vortices in swept-wing flows
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1985
• The laminar-turbulent transition zone in the boundary layer
  Progress in Aerospace Sciences, 1985
• Some observations of the transition process on the windward face of a long yawed cylinder
  Journal of Fluid Mechanics, 1985