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Observed Structure of Spray Detonations
1.F. A. Williams, Phys. Fluids 4, 1434 (1961).
2.F. A. Williams, Combustion Theory (Addison‐Wesley Publishing Company, Reading, Massachusetts, 1965), p. 147.
3.W. T. Webber, in Eighth International Symposium on Combustion (The Williams and Wilkins Company, Baltimore, 1962), p. 1129.
4.F. B. Cramer, in Ninth International Symposium, on Combustion (Academic Press Inc., New York, 1963), p. 482.
5.E. K. Dabora, K. W. Ragland, and J. A. Nicholls, Astronautica Acta 12, 9 (1966).
6.It has been shown that a tube which is coated with a thin layer of liquid and is filled only with oxygen can also support a two phase detonation. See Ref. 5 and K. W. Ragland, Ph.D. thesis, The University of Michigan (1967).
7.E. K. Dabora, K. W. Ragland, and J. A. Nicholls, in Twelfth Symposium (International) on Combustion (Combustion Institute, Pittsburgh, Pennsylvania) (to be published).
8.E. K. Dabora, Rev. Sci. Instr. 38, 502 (1967).
9.J. S. Pirroni and R. R. Stevens, Rev. Sci. Instr. 38, 382 (1967).
10.K. W. Ragland and R. E. Cullen, Rev. Sci. Instr. 38, 740 (1967).
11.A. A. Ranger and J. A. Nicholls, A.I.A.A. J. (to be published).
12.W. H. Andersen and H. E. Wolf, in Proceedings 5th International Shock Tube Symposium (U.S. Naval Ordinance Laboratory, Silver Spring, Maryland, 1965), p. 1145.
13.O. G. Engle, J. Res. Natl. Bur. Std. (U.S.) 60, 245 (1958).
14.When the dynamic pressure is very low such that it is of the order of the surface tension pressure a different type of breakup is observed, which is termed “bag type” (i.e., the drop inflates like a parachute until it bursts in the center). At still lower dynamic pressures the drop vibrates with increasing amplitude until it breaks up.
15.B. J. Clark, NASA Technical Note D‐2424 (1964).
16.F. A. Williams, in Progress in Astronautics and Rocketry (Academic Press Inc., New York, 1962), Vol. 6, p. 99.
17.Ia. B. Zeldovich, Zh. Eksp. Teor. Fiz. 10, (1940)
17.[NACA TM 1261 (1950)].
18.Ia. B. Zeldovich and A. S. Kompaneets, Theory of Detonation (Academic Press Inc., New York, 1960), p. 133.
19.J. A. Fay, Phys. Fluids 2, 283 (1959).
20.F. J. Zeleznik and S. Gordon, NASA Technical Note D 1454 (1962).
21.J. C. Breeze and C. C. Ferriso, Phys. Fluids 7, 1071 (1964).
22.I. I. Glass and G. J. Hall, in Handbook of Supersonic Aerodynamics: Shock Tubes (U.S. Government Printing Office, Washington, D.C., 1959), Vol. 6, Sec. 18.
23.H. Schlichting, Boundary Layer Theory (McGraw‐Hill Book Company, New York, 1960), p. 537.
24.P. B. Gooderum, NACA Technical Note 4243 (1958).
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