Abstract
This manuscript outlines the invention of a miniaturized version of the conventional shock tube and hypersonic shock tunnel that is small enough to be mounted on a table top The shock tube named as Reddy tube works solely with the effect of human force and the driver gas is pressurized by manual action of a plunger rod Test can be conducted within a shock Mach number range of ndash The extension of the Reddy tube into a table top single pulsed hypersonic shock tunnel named as Reddy tunnel proves to be an important input into the field as it can be established as a fraction of the cost of a full fledged facility thereby providing access to such experiments to virtually any person in the experimental aerodynamic community
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