PLIF measurements of temperature and velocity in a reacting supersonic free jet with OH
- 10 January 1994
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Single-shot velocimetry using planar laser-induced fluorescence imaging of nitric oxidePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Nonintrusive, multipoint velocity measurements in high-pressure combustion flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Comparison of NO and OH PLIF temperature measurements in a scramjet model flowfieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Instantaneous planar thermometry of shock-heated flows using PLIF of OHPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Instantaneous, two-line temperature imaging of a H2/NO jet in supersonic crossflowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Instantaneous temperature and concentration imaging in supersonic air flow behind a rear-facing step with hydrogen injectionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Electronic quenching of highly rotationally excited OH(A 2Σ, ν′=0, 1) by H2OChemical Physics Letters, 1988
- Radiative lifetimes and quenching rate coefficients for directly excited rotational levels of OH (A 2Σ+,v′=0)The Journal of Chemical Physics, 1982