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The shock tube results exhibited a significantly higher compressive strength.
A new shock tube with long drift section is proposed.
The main component of this device is a contoured shock tube, which consists of a micro shock tube and an expanded nozzle.
Ignition delay times are measured using both a shock tube and a rapid compression machine.
In present experimental studies, a micro shock tube was designed to investigate the shock wave propagation.
A shock tube setup is then utilized for test the performance of the fabricated pressure sensors.
The mechanism of the Richtmyer-Meshkov instability was experimentally studied in a vertical rectangular shock tube.
Initial shock tube measurements place the absolute accuracy of the thermometer within ∼2% to 1000 K.
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A dedicated shock-tube has been designed and tested to assess calibration performances.
Details on the relatively new high-pressure shock-tube facility are also provided.
It has been validated using available literature data including flow reactor, jet-stirred reactor, shock-tube ignition delay times, shock-tube speciation, flame speed, and flame speciation data.
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