An Overview of NASA Hypersonic Experimental Diagnostic and Instrumentation Technologies for Ground and Flight Testing
Author:
Affiliation:
1. NASA Glenn Research Center
2. NASA Langley Research Center
3. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-7279
Reference12 articles.
1. Dual-Pump Coherent Anti-Stokes Raman Scattering Measurements in a Supersonic Combustor
2. Coherent Anti-Stokes Raman Spectroscopic Thermometry in a Supersonic Combustor
3. Simultaneous velocimetry and thermometry of air by use of nonresonant heterodyned laser-induced thermal acoustics
4. Common-path heterodyne laser-induced thermal acoustics for seedless laser velocimetry
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