Mole-Fraction-Sensitive Imaging of Hypermixing Shear Layers
A theoretical model that determines the optimum excitation frequency for obtaining a fluorescence signal with a strong dependence on fuel mole fraction is presented for supersonic fuel-air compressible mixing studies. The challenge associated with this is to maintain a high sensitivity to fuel mole fraction with minimal sensitivity to temperature and pressure in a flow with large temperature variations and pressure gradients. The results of the model are applied to the mixing region behind...[Show more]
|Collections||ANU Research Publications|
|Source:||Journal of Propulsion and Power|
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