Author:
Baek Seung-Cheol,Kwon Soon-Bum,Lee Byeong-Eun
Publisher
Springer Science and Business Media LLC
Reference12 articles.
1. Addy, A. L., 1981, “Effects of Axisymmetric Sonic Nozzle Geometry on Mach Disk Characteristics, ”AIAA Journal, Vol. 19, No. l, pp. 121–122.
2. Chang, I. S. and Chow, W. L., 1974, “Mach Disk from Underexpanded Axisymmetric Nozzle Flow,”AIAA Journal, Vol. 12, No. 8, pp. 1079–1082.
3. Crist, S., Sheerman, P. M. and Glass, D. R. 1966, “Study of the Highly Underexpanded Sonic Jet,”AIAA Journal, Vol.4, No. 1, pp. 68–71.
4. Crowe, J. J., 1942, “Divergent Nozzle Tips for Economical Oxygen Cutting,”Journal of Weld, Vol. 21. pp. 34–40.
5. Davidor, W. and Penner, S. S., 1971, “Shock Standoff Distances and Mach-Disk Diameters in Underexpanded Sonic Jets, ”AIAA Journal, Vol. 9, No. 8, pp. 1651–1653.
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