NASA NTRS · 19920064407
Measured rotational and vibrational temperature differences in arc jet shock layers
Abstract
Shock-layer-radiation emission spectra from the first negative system of the nitrogen molecular ion N2(+) are analyzed over the wavelength region between 370 and 430 nm. The shock layer is produced by a blunt body placed in the expanded flow from an arc heater employing either pure nitrogen or a nitrogen-oxygen air mixture. A rotational temperature is obtained from analysis of (0,1) band emission from N2(+). Vibrational temperatures are extracted from population distributions obtained through spectral fitting of the N2(+) (B-X) band sequences. Rotational temperatures up to 9500 K near the front of the shocks are determined for different energy and flow conditions. The rotational temperatures are found to be lower than those obtained for vibration confirming previous measurements and contrary to expectation based on theory.
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Blackwell, Harvel E., Scott, Carl D.. 1992-07-01. Measured rotational and vibrational temperature differences in arc jet shock layers. https://ntrs.nasa.gov/citations/19920064407
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