The design of a 50-inch-diameter, continuous-flow, Mach 10-12 wind tunnel, currently operating at Mach 10 only, is described and related operational experience discussed. The tunnel is equipped with an axisymmetric, contoured nozzle and with a fast model injection/ retraction system. Control and data readout systems are described.
PUBLICATION REVIEWThis report has been reviewed and publication is approved.
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