StanShock: a gas-dynamic model for shock tube simulations with non-ideal effects and chemical kinetics
Author:
Funder
Air Force Office of Scientific Research
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-019-00935-x.pdf
Reference42 articles.
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2. Petersen, E.L., Hanson, R.K.: Nonideal effects behind reflected shock waves in a high-pressure shock tube. Shock Waves 10, 405–420 (2001). https://doi.org/10.1007/PL00004051
3. Pang, G.A., Davidson, D.F., Hanson, R.K.: Experimental study and modeling of shock tube ignition delay times for hydrogen/oxygen/argon mixtures at low temperatures. Proc. Combust. Inst. 32, 181–188 (2009). https://doi.org/10.1016/j.proci.2008.06.014
4. Davidson, D.F., Hanson, R.K.: Recent advances in shock tube/laser diagnostic methods for improved chemical kinetics measurements. Shock Waves 19, 271–283 (2009). https://doi.org/10.1007/s00193-009-0203-0
5. Hong, Z., Pang, G., Vasu, S., Davidson, D., Hanson, R.: The use of driver inserts to reduce non-ideal pressure variations behind reflected shock waves. Shock Waves 19, 113–123 (2009). https://doi.org/10.1007/s00193-009-0205-y
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