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Coherent anti-Stokes Raman scattering was used to measure nitrogen single-pulse spectra at the entrance and exit area of a thrust nozzle. Thermodynamic nonequilibrium effects were proved at the exit of the hypersonic nozzle, belonging to an air-breat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::32c5716959ae52c153406c57494dd380
https://elib.dlr.de/964/
https://elib.dlr.de/964/