STN, Shock Tube and Nozzle Calculations for Equilibrium Air

R.M. Krek and P.A. Jacobs
Department of Mechanical Engineering
The University of Queensland
St. Lucia, Qld, 4072, Australia
February 1993

In PDF format or as individual JPEG pages:

• Cover page
• Title, abstract
• Nomenclature
• Introduction, Incident Shock
• Reflected Shock
• Nozzle-Supply Condition
• Nozzle-Throat Condition, Nozzle Exit-Plane Conditioon
• Using the STN Program
• References
• Appendix (stn.h, see source code below)
• Figure 1
• Figures 2 and 3
• Fortran Source Code: stn.for