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NASA NTRS · 19660028030

Electronic Effects in Expansive Flow Under Hypersonic Conditions

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Abstract

Plasma effects in hypersonic shock tunnel nozzle using air

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ELECTRIC PROPERTY PLASMA FLOW HYPERSONIC FLOW SHOCK TUNNEL

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Bloom, M. H.. 1966-01-01. Electronic Effects in Expansive Flow Under Hypersonic Conditions. https://ntrs.nasa.gov/citations/19660028030

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