1977
DOI: 10.1016/0010-2180(77)90091-8
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The effect of electrohydrodynamic boundary layers on heat transfer from flame gases

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Cited by 3 publications
(3 citation statements)
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“…As shown in Figure 2, an aerodynamically stagnant layer of gas formed between the flowing plume and the sampler tip (20,15,16,(38)(39)(40). Formation of a space-charge sheath or electrical double layer in contact with the sampler was also probable (40)(41)(42)(43)(44). This composite boundary layer was in thermal contact with the relatively cool sampler.…”
Section: Resultsmentioning
confidence: 98%
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“…As shown in Figure 2, an aerodynamically stagnant layer of gas formed between the flowing plume and the sampler tip (20,15,16,(38)(39)(40). Formation of a space-charge sheath or electrical double layer in contact with the sampler was also probable (40)(41)(42)(43)(44). This composite boundary layer was in thermal contact with the relatively cool sampler.…”
Section: Resultsmentioning
confidence: 98%
“…As the flowing plasma plume approached the sampler, the plume gas was deflected around the blunt sampler tip. As shown in Figure 2, an aerodynamically stagnant layer of gas formed between the flowing plume and the sampler tip (10, 15,16,[38][39][40]. Formation of a space-charge sheath or electrical double layer in contact with the sampler was also probable (40)(41)(42)(43)(44).…”
Section: Resultsmentioning
confidence: 99%
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