Turbulent Boundary-Layer Flow Separation Measurements Using Holographic Interferometry
Author:
Affiliation:
1. Aerospace Research Laboratories, Wright-Patterson Air Force Base, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49413
Reference5 articles.
1. Application of Dual Hologram Interferometry to Wind-Tunnel Testing
2. An Experimental Investigation of Turbulent Transonic Viscous-Inviscid Interactions
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2. A perspective on a quarter century of CFD research;11th Computational Fluid Dynamics Conference;1993-07-06
3. Measurements of swept shock wave/turbulent boundary-layer interactions by holographic interferometry;20th Fluid Dynamics, Plasma Dynamics and Lasers Conference;1989-06-12
4. Holographic measurements of transition and turbulent bursting in supersonic axisymmetric boundary layers;AIAA Journal;1988-12
5. Holographic Interferometry or Fringe Interpretation;Springer Series in Optical Sciences;1985
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