High Mach Number Scramjet Test Flows in the X3 Expansion Tube
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Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-16835-7_58
Reference8 articles.
1. Doolan, C.J., Morgan, R.G.: A two-stage free-piston driver. Shock Waves 9, 239–249 (1999)
2. Morgan, R.G.: Free-Piston Driven Expansion Tubes. In: Ben-Dor, G., Igra, O., Elperin, T. (eds.) Handbook of Shock Waves, Vol 1, chap. 4.3, pp. 603–622. Academic Press (2001)
3. Gildfind, D.E.: Development of High Total Pressure Scramjet Flow Conditions using the X2 Expansion Tube. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland, Brisbane (2012)
4. McGilvray, M., Kirchhartz, R., Jazra, T.: Comparison of mach 10 scramjet measurements from different impulse facilities. AIAA Journal 48(8), 1647–1651 (2010)
5. Zander, F.: Personal communication (2012)
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Scramjet test flow reconstruction for a large-scale expansion tube, Part 1: quasi-one-dimensional modelling;Shock Waves;2017-11-29
2. X3 expansion tube driver gas spectroscopy and temperature measurements;Shock Waves;2017-11-17
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