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Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. A shock tube is a device used primarily to study gas phase combustion reactions. Shock tubes (and related impulse facilities: shock tunnels, expansion tubes, and expansion tunnels) can also be used to study aerodynamic flow under a wide range of temperatures and pressures that are difficult to obtain in other types of testing facilities. A simple shock tube is a tube, rectangular or circular in cross-section, usually constructed of metal, in which a gas at low…mehr

Produktbeschreibung
Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. A shock tube is a device used primarily to study gas phase combustion reactions. Shock tubes (and related impulse facilities: shock tunnels, expansion tubes, and expansion tunnels) can also be used to study aerodynamic flow under a wide range of temperatures and pressures that are difficult to obtain in other types of testing facilities. A simple shock tube is a tube, rectangular or circular in cross-section, usually constructed of metal, in which a gas at low pressure and a gas at high pressure are separated using some form of diaphragm, see for instance texts by Soloukhin, Gaydon and Hurle, and Bradley. This diaphragm suddenly bursts open under predetermined conditions to produce a wave propagating through the low pressure section. The shock that eventually forms increases the temperature and pressure of the test gas and induces a flow in the directionof the shock wave. Observations can be made in the flow behind the incident front or take advantage of the longer testing times and vastly enhanced pressures and temperatures behind the reflected wave.