PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Oddities in determining burning rate on basis of closed vessel tests of single base propellant

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The proper determination of parameter values defining the dependence of the burning rate r of smokeless propellant on gas pressures p surrounding the burning grains constitutes one of the goals of experimental pyrostatic (closed vessel) testing. The aim of the hereby paper is the analysis of results of experimental closed vessel tests realized in the context of isolating possible oddities in determining the relation r(p). During the experimental tests, a single base propellant with grains of different or similar combustible layer thickness e1 was burned while implementing identical or various loading conditions. Identical ignition systems were used in both instances. The results of experimental tests and theoretical analysis performed permit a more complete verification of the assumptions with regard to proper realization of pyrostatic comparative tests and prove additionally that closed vessel tests should be focused in the direction of “dedicated” tests.
Rocznik
Strony
313--321
Opis fizyczny
Bibliogr. 26 poz., rys.
Twórcy
  • Military University of Technology, Faculty of Mechatronics and Aerospace, Warsaw, Poland
Bibliografia
  • 1. Assovskii I.G., Zakirov Z.G., Leipunskii O.I., 1983, Effect of ignition on fuel combustion, Combustion, Explosion, Shock Waves, 19, 1, 37-42
  • 2. Assovskii I.G., Zakirov Z.G., Leipunskii O.I., 1986, Ignition and combustion of propellant in a radiating gas flow, Combustion, Explosion, Shock Waves, 22, 6, 658-663
  • 3. Baer P.G., 1979, Practical interior ballistic analysis of guns, Progress in Astronautics and Aeronautics, AIAA, 66, 37-66
  • 4. Cieślak K., Ostaszewski D., Książczak A., 2011, Analysis of the structure of seven-perforation propellant grain for medium-calibre ammunition and single-perforation for small-calibre ammunition (in Polish), Proceedings of 18th International Conference on Development Production and Maintenance of Weapons Systems, Pułtusk, Poland, 439-445
  • 5. Corner J., 1950, Theory of the Interior Ballistics of Guns, John Wiley & Sons, Inc., New York
  • 6. Eisenrich N., Fischer T.S., Langer G., Kelzenberg S., Weiser V., 2002, Burn rate models for gun propellants, Propellants, Explosion, Pyrotechnics, 27, 3, 142-149
  • 7. Grune D., Hensel D., 1993, Burning behavior of high energy solid propellants in closed vessels at high loading densities, Proceedings of the 14th International Symposium on Ballistics, Quebec, Canada, 223-229
  • 8. Jeunieau L., Lefebvre M.H., Papy A., Pirlot M.C., Guillaume P., Reynaud Ch., 2002, Closed vessel test: influence of the ignition method on the combustion rate, 33rd International Annual Confernce of ICT, Karlsruhe, Germany
  • 9. Khomenko Yu. P., Shirokov V.M., 2006, Determining the unsteady combustion behaviour of propellants from results of closed-bomb testing, Combustion, Explosion, Shock Waves, 42, 2, 149-157
  • 10. Khristenko Yu. F., 2001, Experimental methods for studying the combustion of granular powder in a broad range of process parameters, Combustion, Explosion, Shock Waves, 27, 1, 72-77
  • 11. Leciejewski Z.K., 2007,Singularities of burning rate determination of fine-grained propellants, Proceedings of 23rd International Symposium on Ballistics, Tarragona, Spain, Vol. I, 369-376
  • 12. Leciejewski Z.K., 2008a, Criticism of linear form of burning rate law with reference to conventional fine-grained propellants, Proceedings of the 7th International Armament Conference SAAT’2008, Pułtusk, Poland, 191-200
  • 13. Leciejewski Z.K., 2008b, Experimental study of possibilities for employment of linear form of burning rate law to characterise the burning process of fine-grained propellants, Central European Journal of Energetic Materials, 5, 1, 45-61
  • 14. Leciejewski Z.K., Surma Z., 2011, Effect of application of various ignition conditions in closed vessel tests on burning rate calculation of a fine-grained propellant, Combustion, Explosion and Shock Waves, 47, 2, 209-216
  • 15. Leonov G.N., 2008, Some aspects of the effect of the porosity of the condensed phase on the combustion of nitrocellulose propellants, Combustion, Explosion, Shock Waves, 44, 5, 547-551
  • 16. Papliński A., 2002, Numerical analysis of initiation of transient combustion process in granular beds of propellant, Proceedings of the 4th International Armament Conference SAAT’2002, Waplewo, Poland, 87
  • 17. Serebryakov M., 1949, Internal Ballistics (in Russian), Oborongiz, Moscow
  • 18. Smoleński D., 1979, Combustion of Explosives (in Polish), MoD, Warsaw
  • 19. STANAG 4115 LAND (Ed. 2), 1997, Definition and Determination of Ballistic Properties of Gun Propellants, Military Agency for Standardization, Brussels
  • 20. STANAG 4367 LAND (Ed. 2), 2000, Thermodynamic Interior Ballistic Model with Global Parameters, Military Agency for Standardization, Brussels
  • 21. Taylor M.J., Woodley C.R., Fuller S.R., Gilbert S., Gransden J.I., 2008, Consideration of the ignition delay of gun propellants, Proceedings of the 24th International Symposium on Ballistics, New Orleans, USA, Vol. I, 59-66
  • 22. Torecki S., Leciejewski Z.K., Surma Z., Ciepielski S., Wójcik R., 1999, Complex investigation of thermodynamic properties of propellant gases and real burning rate of propellants and revision of internal ballistic formulas, Report No. OT00A00811, Military University of Technology, Warsaw
  • 23. Tuomainen A.H., 1996, The thermodynamic model of interior ballistics, Thesis, Acta Polytechnica Scandinavica, Applied Physics Series, 205, University of Helsinki
  • 24. Wang G., 1993, Experimental research on porous propellant with high burning rate, Proceedings of the 14th International Symposium on Ballistics, Quebec, Canada, 399-405
  • 25. Woodley C., Taylor M., Wheal H., 2007, Boundary layer modelling of the heat transfer process from igniters to energetic materials, Proceedings of 23rd International Symposium on Ballistics, Tarragona, Spain, Vol. I, 295-302
  • 26. Zel’dovich Ya.B., 1982, Theory of Combustion of Propellant and Explosives (in Russian), Nauka, Moscow
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-32da1419-e47c-4435-8642-c89f1395dba3
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.