Analysis of an induction blowdown supersonic tunnel

Jerold M. Bidwell
naca-tn-2040
Apr 1950


General ejector equations and certain assumptions with regard to flow conditions and pressure losses are used to calculate the running times for one type of induction blowdown supersonic tunnel for Mach numbers of 1 to 2 and for reservoir pressures of 2 to 4 atmospheres.

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