Simplifications of the RELIEF flow tagging system for laboratory use
Author:
Affiliation:
1. Princeton University, NJ
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-356
Reference13 articles.
1. Velocity measurements by vibrational tagging and fluorescent probing of oxygen
2. W.R. Lempert, 8.Zhang, R.B. Miles, and J.P. L J. opt. so=. m 82. p.715 (1990).
3. On the possibility of measuring gas concentrations by stimulated anti‐Stokes scattering
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1. Observation of vibrational relaxation dynamics in X3Sigma(-)g oxygen following stimulated Raman excitation to the v=1 level - Implications for the RELIEF flow tagging technique;34th Aerospace Sciences Meeting and Exhibit;1996-01-15
2. Progress in laser spectroscopic techniques for aerodynamic measurements - An overview;AIAA Journal;1993-03
3. Fundamental turbulence measurements by relief flow tagging;AIAA Journal;1993-03
4. Stokes seeding of a Raman shifting cell for use in RELIEF velocimetry;31st Aerospace Sciences Meeting;1993-01-11
5. Progress in laser-spectroscopic techniques for aerodynamic measurements - An overview;29th Aerospace Sciences Meeting;1991-01-07
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