Modeling mass entrainment in a quasi-one-dimensional shock tube code

AIAA Journal

Volumn 34, Issue 6, 1996, Pages 1291-1293

  Doolan, C J ^a,b   Jacobs, P A ^a,b  

^a UNIVERSITY OF QUEENSLAND   (Australia)

^b Department of Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0041717286     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13227     Document Type: Article

References (9)

1. Jacobs, P. A., "Quasi-One-Dimensional Modeling of a Free-Piston Shock Tunnel," AIAA Journal, Vol. 32, No. 1, 1994, pp. 137-145.
2. Tanj, K., Itoh, K., Takahashi, M., Tanno, H., Komuro, T., and Miyajima, H., "Numerical Study of Free-Piston Shock Tunnel Performance," Shoct Waves Journal, Vol. 3, No. 4, 1994, pp. 313-319.
3. Sharma, S. P., and Wilson, G. J., "Test-Times in Hypersonic Shock Tubes," AIAA Paper 95-0713, Jan. 1995.
4. Mirels, H., "Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer," AIAA Journal, Vol. 2, No. 1. 1964, pp. 84-93.
5. Watson, R. D., "Generalized Velocities in the Outer Region of Hypersonic Turbulent Boundary Layers," AIAA Journal, Vol. 17, No. 8, 1979, pp. 919-921.
6. Schetz, J. A., Boundary Layer Analysis, Prentice-Hall, Englewood Cliffs, NJ, 1993, pp. 240, 241.
7. Groth, C. P. T., Gottlieb, J. J., and Sullivan, P. A., "Numerical Investigation of High Temperature Effects in UTIAS-RPI Hypersonic Impulse Tunnel," Canadian Journal of Physics, Vol. 69, No. 7, 1991, pp. 897-918.
8. Lacey, J. J., "Experimental Shock Tube Test Time - Turbulent Regime," Proceedings of the 7th Shock Tube Symposium, Univ. of Toronto Press, Toronto, ON, Canada, 1969, pp. 126-142.
9. Fuehrer, R. G., "Measurements of Incident-Shock Test Time and Reflected Shock Pressure at Fully Turbulent Boundary-Layer Test Conditions," Proceedings of the 7th Shock Tube Symposium, Univ. of Toronto Press, Toronto, ON, Canada 1969, pp. 31-59.