The development of atmospheric hypersonic flight and re-entry capabilities requires the characterization of the thermo-chemical state of representative test environments. This study …
Planar laser induced fluorescence (PLIF) 1 is an instantaneous, spatially-resolved optical measurement technique that involves molecular excitation for both quantitative …
LML Cantu, J Grohmann, W Meier, M Aigner - Experimental Thermal and …, 2018 - Elsevier
A gas turbine model combustor for swirling spray flames has been operated at atmospheric pressure with n-hexane, n-dodecane and kerosene Jet A-1. Temperature measurements …
Nitric oxide planar laser-induced fluorescence measurements have been performed in a small-scale scramjet combustor at the University of Virginia Aerospace Research Laboratory …
View Video Presentation: https://doi. org/10.2514/6.2022-0893. vid A femtosecond/ picosecond (fs/ps) coherent anti-Stokes Raman scattering (CARS) model of CO and CO2 is …
View Video Presentation: https://doi. org/10.2514/6.2023-0167. vid The current interest in hypersonic flows and the growing importance of plasma applications necessitate the …
WIDECARS measures temperature and mole fractions of most of the major species in ethylene–air flames. One of the issues in implementing this technique is fitting the …
The development of heat shields for hypersonic flight and atmospheric re-entry requires experimental data obtained in relevant high-enthalpy flow environments. Measurements in …
Width-increased dual-pump enhanced coherent anti-Stokes Raman spectroscopy (WIDECARS) measurements were used to determine the temperature and major species …