A procedure to compute influence of experimental shot-to-shot variation on expansion tube test flow properties
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-019-00903-5.pdf
Reference30 articles.
1. Gildfind, D.E., Morgan, R.G., Jacobs, P.A.: Expansion tubes in Australia. In: Igra, O., Seiler, F. (eds.) Experimental Methods of Shock Wave Research. Shock Wave Science and Technology Reference Library, vol. 9. Springer (2016). https://doi.org/10.1007/978-3-319-23745-9_13
2. Jacobs, P.A.: Quasi-one-dimensional modeling of a free-piston shock tunnel. AIAA J. 32(1), 137–145 (1994). https://doi.org/10.2514/3.11961
3. Gollan, R., Jacobs, P.: About the formulation, verification and validation of the hypersonic flow solver Eilmer. Int. J. Numer. Methods Fluids 73, 19–57 (2013). https://doi.org/10.1002/fld.3790
4. Gildfind, D., Jacobs, P., Morgan, R., Chan, W., Gollan, R.: Scramjet test flow reconstruction for a large-scale expansion tube, part 1: quasi-one-dimensional modelling. Shock Waves 28(4), 877–897 (2017). https://doi.org/10.1007/s00193-017-0785-x
5. Gildfind, D., Jacobs, P., Morgan, R., Chan, W., Gollan, R.: Scramjet test flow reconstruction for a large-scale expansion tube, part 2: hybrid CFD analysis. Shock Waves 28(4), 899–918 (2017). https://doi.org/10.1007/s00193-017-0786-9
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