Caldersmith, Graham William2017-12-212017-12-211973b1016426http://hdl.handle.net/1885/13857279 p.enPlasma (Ionized gases)Shock tubesHypersonic wind tunnelsElectromotive forceElectrical effects in a hypersonic nozzle flow plasma197310.25911/5d6e4b23b34d42017-11-22