1. H. Mirels, Aerospace Corporation Report, TDR-169(3230-12)TN-5 (1962). [This report includes some more detailed discussion.]
2. A Theoretical and Experimental Study of Shock-Tube Flows
3. R. N. Hollyer, Jr., “A Study of Attenuation in the Shock Tube,” Engineering Research Institute, University of Michigan (1953).
4. R. L. Trimpi and N. B. Cohen, NACA TN 3375 (1955).
5. H. Mirels, NACA Report 1333 (1957).