Show simple item record

Observed Structure of Spray Detonations

dc.contributor.authorRagland, Kenneth W.en_US
dc.contributor.authorDabora, Eliahou K. (Eliahou Khedhoory)en_US
dc.contributor.authorNicholls, James Arthuren_US
dc.date.accessioned2010-05-06T23:36:23Z
dc.date.available2010-05-06T23:36:23Z
dc.date.issued1968-11en_US
dc.identifier.citationRagland, K. W.; Dabora, E. K.; Nicholls, J. A. (1968). "Observed Structure of Spray Detonations." Physics of Fluids 11(11): 2377-2388. <http://hdl.handle.net/2027.42/71352>en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/71352
dc.description.abstractThe propagation of a detonation wave in a tube containing a single stream of 2600‐μ‐diam diethylcyclohexane droplets dispersed in gaseous oxygen has been studied with streak and space resolved photography, special pressure transducers, and thin‐film heat‐transfer gauges. The detonation wave, which reached a velocity of 4100 ft/sec, consisted of a planar shock front followed by secondary shocks and a gradual decrease in pressure as heat is added. A detailed history of an individual drop within the reaction zone is presented. Under the observed conditions a 2600‐μ‐drop disintegrates continuously over a period of 500 μsec. Combustion is initiated in the wake of the drops at 65 μsec after the passage of the shock with the reaction zone considered completed in 670 μsec. One‐dimensional equations for a two‐phase Chapman‐Jouguet detonation wave with mass and heat addition within the reaction zone, and momentum and heat transfer out of the reaction zone are derived. Comparison of the experiments with the theoretical prediction yields a reasonable agreement.en_US
dc.format.extent3102 bytes
dc.format.extent1102430 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.publisherThe American Institute of Physicsen_US
dc.rights© The American Institute of Physicsen_US
dc.titleObserved Structure of Spray Detonationsen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelPhysicsen_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumGas Dynamics Laboratories, Department of Aerospace Engineering The University of Michigan, Ann Arbor, Michiganen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/71352/2/PFLDAS-11-11-2377-1.pdf
dc.identifier.doi10.1063/1.1691827en_US
dc.identifier.sourcePhysics of Fluidsen_US
dc.identifier.citedreferenceF. A. Williams, Phys. Fluids 4, 1434 (1961).en_US
dc.identifier.citedreferenceF. A. Williams, Combustion Theory (Addison‐Wesley Publishing Company, Reading, Massachusetts, 1965), p. 147.en_US
dc.identifier.citedreferenceW. T. Webber, in Eighth International Symposium on Combustion (The Williams and Wilkins Company, Baltimore, 1962), p. 1129.en_US
dc.identifier.citedreferenceF. B. Cramer, in Ninth International Symposium, on Combustion (Academic Press Inc., New York, 1963), p. 482.en_US
dc.identifier.citedreferenceE. K. Dabora, K. W. Ragland, and J. A. Nicholls, Astronautica Acta 12, 9 (1966).en_US
dc.identifier.citedreferenceIt 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).en_US
dc.identifier.citedreferenceE. K. Dabora, K. W. Ragland, and J. A. Nicholls, in Twelfth Symposium (International) on Combustion (Combustion Institute, Pittsburgh, Pennsylvania) (to be published).en_US
dc.identifier.citedreferenceE. K. Dabora, Rev. Sci. Instr. 38, 502 (1967).en_US
dc.identifier.citedreferenceJ. S. Pirroni and R. R. Stevens, Rev. Sci. Instr. 38, 382 (1967).en_US
dc.identifier.citedreferenceK. W. Ragland and R. E. Cullen, Rev. Sci. Instr. 38, 740 (1967).en_US
dc.identifier.citedreferenceA. A. Ranger and J. A. Nicholls, A.I.A.A. J. (to be published).en_US
dc.identifier.citedreferenceW. H. Andersen and H. E. Wolf, in Proceedings 5th International Shock Tube Symposium (U.S. Naval Ordinance Laboratory, Silver Spring, Maryland, 1965), p. 1145.en_US
dc.identifier.citedreferenceO. G. Engle, J. Res. Natl. Bur. Std. (U.S.) 60, 245 (1958).en_US
dc.identifier.citedreferenceWhen 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.en_US
dc.identifier.citedreferenceB. J. Clark, NASA Technical Note D‐2424 (1964).en_US
dc.identifier.citedreferenceF. A. Williams, in Progress in Astronautics and Rocketry (Academic Press Inc., New York, 1962), Vol. 6, p. 99.en_US
dc.identifier.citedreferenceIa. B. Zeldovich, Zh. Eksp. Teor. Fiz. 10, (1940) [NACA TM 1261 (1950)].en_US
dc.identifier.citedreferenceIa. B. Zeldovich and A. S. Kompaneets, Theory of Detonation (Academic Press Inc., New York, 1960), p. 133.en_US
dc.identifier.citedreferenceJ. A. Fay, Phys. Fluids 2, 283 (1959).en_US
dc.identifier.citedreferenceF. J. Zeleznik and S. Gordon, NASA Technical Note D 1454 (1962).en_US
dc.identifier.citedreferenceJ. C. Breeze and C. C. Ferriso, Phys. Fluids 7, 1071 (1964).en_US
dc.identifier.citedreferenceI. 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.en_US
dc.identifier.citedreferenceH. Schlichting, Boundary Layer Theory (McGraw‐Hill Book Company, New York, 1960), p. 537.en_US
dc.identifier.citedreferenceP. B. Gooderum, NACA Technical Note 4243 (1958).en_US
dc.owningcollnamePhysics, Department of


Files in this item

Show simple item record

Remediation of Harmful Language

The University of Michigan Library aims to describe library materials in a way that respects the people and communities who create, use, and are represented in our collections. Report harmful or offensive language in catalog records, finding aids, or elsewhere in our collections anonymously through our metadata feedback form. More information at Remediation of Harmful Language.

Accessibility

If you are unable to use this file in its current format, please select the Contact Us link and we can modify it to make it more accessible to you.