Measurements of Sphere Drag from Hypersonic Continuum to Free-Molecule Flow

Measurements of Sphere Drag from Hypersonic Continuum to Free-Molecule Flow

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The results of tests conducted in a Hotshot-type wind tunnel with air at stagnation temperatures of approximately 2500* K and 9000* K and with helium at stagnation ion ion temperatures varying from 1600* K to 4000* K.