1. Influence of surface roughness on the transition from regular to Mach reflection in pseudo-steady flows
2. Domains and boundaries of non-stationary oblique shock-wave reflexions. 1. Diatomic gas
3. L. F. Henderson (private communication).
4. See National Technical Information Service Document No. ADB 014070∕LP (Air Force Weapons Laboratory, Kirtland Air Force Base, Report No. AFWL-TR-76-183, 1976, by M. A. Fry, R. E. Durrett, G. P. Ganong, D. A. Matuska, M. Stucker, B. S. Chambers, C. E. Needham, and C. D. Westmoreland). Copies may be ordered from the National Technical Information Service, Springfield, Virginia 22161. The price is $11.95 plus a $3.00 handling fee. All orders must be prepaid.
5. C. E. Needham, H. J. Happ, and D. F. Dawsom, inShock Waves and Shock Tubes, edited by D. Bershader and R. Hanson (Stanford U.P., Stanford, CA, 1986), pp. 407–413.