Unsteady shock propagation in a steady flow nozzle expansion

Journal of Fluid Mechanics

Volumn 241, Issue 24, 1992, Pages 525-548

  Mudford, N R ^b  

^a UNIVERSITY OF QUEENSLAND   (Australia)

^b UNIVERSITY OF NEW SOUTH WALES   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 3843109023     PISSN: 00221120     EISSN: 14697645     Source Type: Journal    
DOI: 10.1017/S0022112092002143     Document Type: Article

References (15)

1. Ackroyd, J. A. D. 1964 Studies on the running time in a shock tube and shock tunnel. PhD thesis, University of London.
2. Davies L. 1964 Bow-shock establishment and stagnation point pressure measurements for a blunt-nosed body at supersonic speeds. Natl Phys. Lab. Aero Rep. 1098.
3. Hornung H. G. & Sandeman, R. J. 1974 Interferometry of radiating argon flow over blunt bodies. J. Phys. D: Appl. Phys. 7, 920.
4. Liepmann, H. W. & Roshko, A. 1957 Elements of Gas Dynamics, p. 149. J. Wiley & Sons.
5. Logan P. F., Stalker R. J. & McIntosh M. K. 1977 A shock tube study of radiative energy loss from an argon plasma. J. Phys. D: Appl. Phys. 10, 323.
6. Macrossan, M. N. 1990 Hypervelocity flow of dissociating nitrogen downstream of a blunt nose. J. Fluid Mech. 217, 167.
7. Mudford, N. R. 1976 The production of pulsed nozzle flows in a shock tube. PhD thesis, Australian National University, Canberra.
8. Mudford, N. R. & Stalker, R. J. 1976 The production of pulsed nozzle flows in a shock tube. AIAA paper 76–357. (Presented at AIAA 9th Fluid and Plasma Dynamics Conference, San Diego.)
9. Mudford, N. R. & Stalker R. J. 1980 Hypersonic nozzles for high enthalpy non-equilibrium flow. Aero. Q. 31, 113.
10. Oertel, H. 1970 Non-reflected shock tunnel test times. Proc. 7th Intl Shock Tube Symp. (ed. I. I. Glass), p. 80. University of Toronto Press.
11. Rudinger, G. 1955 Wave Diagrams for Nonsteady Flow in Ducts, pp. 18–33. New York Van Nostrand.
12. Smith, C. E. 1966 The starting process in a hypersonic nozzle. J. Fluid Mech. 24, 625.
13. stalker, R. J. 1972 Development of a hypervelocity wind tunnel. Aero. J. R. Aero. Soc. 76, 374.
14. Stalker, R. J. 1980 Shock tunnel measurements of ionization rates in hydrogen. AIAA J. 18, 478.
15. Stalker, R. J. & Mudford, N. R. 1973 Starting process in the nozzle of a non-reflected shock tunnel. AIAA J. 11, 265.