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High-speed imaging of inhomogeneous ignition in a shock tube

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Abstract

Homogeneous and inhomogeneous ignition of real and surrogate fuels were imaged in two Stanford shock tubes, revealing the influence of small particle fragmentation. n-Heptane, iso-octane, and Jet A were studied, each mixed in an oxidizer containing 21% oxygen and ignited at low temperatures (900–1000 K), low pressures (1–2 atm), with an equivalence ratio of 0.5. Visible images (350–1050 nm) were captured through the shock tube endwall using a high-speed camera. Particles were found to arrive near the endwalls of the shock tubes approximately 5 ms after reflection of the incident shock wave. Reflected shock wave experiments using diaphragm materials of Lexan and steel were investigated. Particles collected from the shock tubes after each experiment were found to match the material of the diaphragm burst during the experiment. Following each experiment, the shock tubes were cleaned by scrubbing with cotton cloths soaked with acetone. Particles were observed to fragment after arrival near the endwall, often leading to inhomogeneous ignition of the fuel. Distinctly more particles were observed during experiments using steel diaphragms. In experiments exhibiting inhomogeneous ignition, flames were observed to grow radially until all the fuel within the cross section of the shock tube had been consumed. The influence of diluent gas (argon or helium) was also investigated. The use of He diluent gas was found to suppress the number of particles capable of causing inhomogeneous flames. The use of He thus allowed time history studies of ignition to extend past the test times that would have been limited by inhomogeneous ignition.

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Acknowledgements

This material is based upon work supported by the U.S. Army Research Laboratory and the U.S. Army Research Office under contract/Grant Number W911NF-13-1-0206.

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Correspondence to A. M. Tulgestke.

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Communicated by G. Ciccarelli.

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Tulgestke, A.M., Johnson, S.E., Davidson, D.F. et al. High-speed imaging of inhomogeneous ignition in a shock tube. Shock Waves 28, 1089–1095 (2018). https://doi.org/10.1007/s00193-018-0824-2

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  • DOI: https://doi.org/10.1007/s00193-018-0824-2

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