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NASA NTRS · 19670032713

Electronic effects in expansive flow under hypersonic conditions.

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Abstract

Plasma effects in nozzle flow of hypersonic shock tunnel using air, obtaining electron density profile

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NOZZLE FLOW PLASMA FLOW ELECTRON DENSITY SHOCK TUNNEL

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Bloom, M. H.. 1966-10-01. Electronic effects in expansive flow under hypersonic conditions.. https://ntrs.nasa.gov/citations/19670032713

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