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Theoretical and Experimental Study on Detonation Wave Propagation in Cylindrical High Explosive Charges with a Wave-shaper

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Języki publikacji
EN
Abstrakty
EN
The use of a cylindrical high-explosive charge with a wave-shaper is an efficient way to obtain an ultra-high pressure and a convergent detonation wave. An analysis of flow fields corresponding to the regular and Mach reflection of detonation waves in a cylindrical high-explosive charge with a wave-shaper is presented in this paper. The pressure, flow velocity and triple point growth angle of the Mach stem were calculated. The Mach stem height was also determined by using the modified Whitham method. The results show that the Mach stem height rises from zero at the critical angle of Mach reflection and changes to the Chapman-Jouguet detonation state with the propagation of the detonation waves. Shock indentation experiments were conducted, in which a wave-shaper was used in a cylindrical high-explosive charge to form Mach reflection detonation waves. The results showed that the discrepancy between the experimental results and the theoretical calculations was less than 15%, which proves the validity of the proposed theoretical model.
Rocznik
Strony
658--676
Opis fizyczny
Bibliogr. 26 poz., rys., tab.
Twórcy
autor
  • School of Mechanical Engineering, Nanjing University of Science and Technology, Xiaolingwei 200, Nanjing 210094, China
autor
  • School of Mechanical Engineering, Nanjing University of Science and Technology, Xiaolingwei 200, Nanjing 210094, China
autor
  • School of Mechanical Engineering, Nanjing University of Science and Technology, Xiaolingwei 200, Nanjing 210094, China
autor
  • School of Mechanical Engineering, Nanjing University of Science and Technology, Xiaolingwei 200, Nanjing 210094, China
autor
  • School of Engineering, University of Liverpool, Brownlow Street, Liverpool L69 3GQ, UK
Bibliografia
  • [1] Dowker J.S., Quantum Mechanics on Group Space and Huygens’ Principle, Ann.Phys. (Amsterdam, Neth.), 1971, 62(2), 361-382.
  • [2] Zhu C.S., Huang Z.X., Zu X.D., Xiao Q.Q., Mach Wave Control in Explosively Formed Projectile Warhead, Propellants Explos. Pyrotech., 2014, 39(6), 909-915.
  • [3] Zhang Y.G., Zhang X.F., He Y., Qiao L., Detonation Wave Propagation in Shaped Charges with Large Wave-shaper, 27th Int. Symp. Ballistics, Freiberg, Germany, 2013, 770-782.
  • [4] Al’tshule L.V.R, Zubarev V.N., Telegin G.S., Supercompressed Detonation Waves in Condensed Explosives, Combust. Explos. Shock Waves (Engl. Transl.), 1974, 10(5), 648-652.
  • [5] Dunne B.B., Mach Reflection of Detonation Waves in Condensed High Explosive, Phys. Fluids, 1961, 4(7), 918-933.
  • [6] Dunne B.B., Mach Reflection of Detonation Waves in Condensed High Explosive II, Phys. Fluids, 1964, 7(10), 1707-1712.
  • [7] Krishnan S., Brochet C., Cheret R., Mach Reflection in Condensed Explosives, Propellants Explos. Pyrotech., 1981, 6(6), 170-172.
  • [8] Trotsyuk A.V., Kudryavtsev A.N., Ivanov M.S., Mach Reflection of Shock and Detonation Waves in Steady Supersonic Chemically Reacting Flows, Proc. Int. Conf. on Recent Advances in Space Technologies, Istanbul, Turkey, 2003, 495-503.
  • [9] Wang L., Mach Stem Height in Pseudo-steady and Unsteady Mach Reflection, Journal of Fudan University (Natural Science), 2010, 49(4), 513-519.
  • [10] Hull L.M., Mach Reflection of Spherical Detonation Waves, Report No. LAUR-93-2080, 1993.
  • [11] Hull L.M., Detonation Propagation and Mach Stem Formation in PBXN-9, Report No. LA-UR-97-3827, 1997.
  • [12] Zhang X.F., Huang Z.X., Qiao L., Detonation Wave Propagation in Double-layer Cylindrical High Explosive Charge, Propellants Explos. Pyrotech., 2011, 36(3), 210-218.
  • [13] Cao B., Yu Z.Y., Chen H.W., An Experimental Investigation on the Loading Performance and Propagation Law of Detonation Mach-waves (in Chinese), Journal of Ballistics, 2000, 12(2), 79-83.
  • [14] Fan B.C., Yang Q.Z., Yang S.H., The Propagation and Interactions of Axisymmetric Detonation Waves (in Chinese), Explosive and Shock Waves, 1984, 4(1), 68-77.
  • [15] Grasso F., Paoli R., An Analytical Study of Mach Reflection in Nonequilibrium Steady Flows, Phys. Fluids, 1999, 11(10), 3150-3167.
  • [16] Chpoun A., Passerel D., Li H., Ben-Dor G., Reconsideration of Oblique Shock Wave Reflections in Steady Flows, Part 1. Experimental Investigation, J. Fluid Mech., 1995, 301, 19-35.
  • [17] Teng H.H., Jiang Z.L., Gasdynamic Characteristics of Toroidal Shock and Detonation Wave Converging, Science in China Series G: Physics and Astronomy, 2005, 48(6), 739-749.
  • [18] Panov K.N., Konmrachkov V.A., Tselikov I.S., Radiographic Study of Interaction of Shock and Detonation Waves in a High Explosive, Combust., Explos. Shock Waves (Engl. Transl.), 2007, 43(3), 365-371.
  • [19] Levin V.A., Manuylovich I.S., Markov V.V., Detonation in Supersonic Flows in Channels with Obstacles, 28th Int. Symp. on Shock Waves, Heidelberg, Germany, 2012, 397-402.
  • [20] Li J., Ning J., Lee J.H.S., Mach Reflection of a ZND Detonation Wave, Shock Waves, 2015, 25(3), 293-304.
  • [21] Sternberg H.M., Piacesi D., Interaction of Oblique Detonation Waves with Iron, Phys. Fluids, 1966, 9(7), 1307-1315.
  • [22] Whitham G.B., A New Approach to Problems of Shock Dynamics. Part I. Twodimension Problem, J. Fluid Mech., 1957, 2(02), 145-171.
  • [23] Whitham G.B., Linear and Nonlinear Waves, Vol. 8, Shock Dynamics, John Wiley & Sons, New York – London – Sydney – Toronto, 1974, pp. 263-311; ISBN 0-471-94090-9.
  • [24] Lambourn B.D., Wright P.W., Mach Interaction of Two Plane Detonation Waves, Proc.4th Symp. on Detonation, Office of Naval Research Arlington, VA, USA, 1965, 142-152.
  • [25] Zhang J.X., Yun S.R., Experimental Investigations of the Mach Reflection in a Condensed Explosive (in Chinese), Explosive and Shock Waves, 1986, 6(3), 208-213.
  • [26] Müller F., Mach-reflection of Detonation Waves in Condensed High Explosives, Propellants Explos. Pyrotech., 1978, 3(4), 115-118.
Typ dokumentu
Bibliografia
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bwmeta1.element.baztech-88107403-5de6-4b28-8ad3-71c6bab2ba2b
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