Nonideal effects behind reflected shock waves in a high-pressure shock tube

By E. Petersen, R. Hanson. 2001

220 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Fluid Flow and Transfer Processes

View Paper: https://www.semanticscholar.org/paper/a6e6e24fbfa2836a2a7c946431b0fd098ab6aa9b

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1. K. Heufer
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Citations in the corpus

• Determination of ignition delay times of different hydrocarbons in a new high pressure shock tube (2010, background): “Without shielding, the penetrating heat loads cause a decreasing signal of the pressure gauges so that lower gradients are determined withanunshieldedgauge[1].Thetemperaturegradientshave beendeterminedassuminganisentropiccompressionbehind the reflected shock caused by the shock attenuation (Eq. 3 [ ”