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Modeling of Solid Propellants Viscoplastic Behavior Using Evolutionary Algorithms

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In the paper an initial attempt to the experimental analysis of viscous effects, characteristic for homogeneous solid rocket fuels is proposed. For this reason uniaxial tensile experiments, carried out on dumbbell homogeneous solid propellants have been chosen. Laboratory tests have been carried out on INSTRON tensile testing machine. Research schedule involved destructive tensile tests with various strain rates. Three different values of strain rates have been taken into consideration. Experimentally obtained hardening curves are presented in suitable diagrams. Basing on obtained results, authors confrm the viscoplastic behavior of studied materials. Essential impact of the applied strain rate on the position of experimental hardening curves is observed. Acquired results are the base for the further stage of investigations of homogeneous solid propellants – the modeling of their physical properties. Additionally, numerical modeling of studied phenomena, using the viscoplastic Chaboche’s model, identifed on the basis of experimental data, is presented. The material parameters of the constitutive law are determined numerically using an evolutionary algorithm procedure. The effciency of the model and the identifcation approach are discussed.
Rocznik
Strony
289--300
Opis fizyczny
Bibliogr. 14 poz.
Twórcy
autor
autor
  • Institute of Machines Design Fundamentals, Warsaw University of Technology, 84 Narbutta St., 02-524 Warsaw, Poland, robertzalewski@wp.pl
Bibliografia
  • [1] Kubota N., Survey of Rocket Propellants and Their Combustion Characteristics, in: Kuo K.K, Summerfield M. (Eds.), Fundamentals of Solid-propellant Combustion, vol. 90, Progress in Astronautics and Aeronautics, AIAA, 1984, pp. 1-52.
  • [2] Jung G., Youn S., Kim B., A Three – Dimensional Nonlinear Viscoelastic Constitutive Model of Solid Propellant, International Journal of Solids and Strucures, 2000, 37, 4715-4732.
  • [3] Renganathan K., Rao B., Jana M., , Failure Pressure Estimations on Solid Propellant Rocket Motor with a Circular Perforated Grain, International Journal of Pressure Vessels and Piping, 1999, 76, 955-963.
  • [4] Bodner S.R., Partom Y., Constitutive Equations for Elastic-viscoplastic Strain hardening Materials, J. Appl. Mech., 1975, 42, 385-9.
  • [5] Buckley C.P., Jones D.C., Glass–rubber Constitutive Model for Amorphous Polymers Near the Glass Transition, Polymer, 1995, 36, 3301–12.
  • [6] Chan K.S., Bodner S.R., Lindholm U.S., Phenomenological Modelling of Hardening and Thermal Recovery in Metals, J. Eng. Mater. Technol., 1988, 110, 1-8.
  • [7] Woźnica K., Dynamique des Structures Elasto-viscoplastique, Memoire d’habilitation a diriger des recherches, Universite des Sciences et Technologies de Lille, Lille 1997.
  • [8] Duszek M.K., Perzyna P., Influence of Kinematic Hardening on Plastic Flow Localization in Damaged Solids, Arch. Mech., 1988, 40(5-6), 595-609.
  • [9] Kłosowski P., Zagubień A., Analysis of Material Properties of Technical Fabric for Hanging Roofs and Pneumatic Shells, Archive of Civil Engineering XLIX, 2003, (3), 277-294.
  • [10] Kłosowski P., Zagubień A., Woznica K., Investigation on Rheological Proprties of Technical Fabric „Panama”, Archive of Applied Mechanics, 2004, 73, 661-681.
  • [11] Argon A.S., A Theory for the Low Temperature Plastic Deformation of Glassy Polymers, Phil. Mag., 1973, 28, 839-65.
  • [12] Bäck T., Evolutionary Algorithms in Theory and Practice, Oxford Univ. Press, New York 1995.
  • [13] Michalewicz Z., Genetic Algorithms + Data Structures = Evolution Programs, Springer Verlag, Berlin, Heidelberg, New York, 1992.
  • [14] Pyrz M., Zalewski R., Application of Evolutionary Algorithms to the Identification of Parameters of New Smart Structures – Preliminary Approach, Machine Dynamics Problems, 2006, 30(2), 136-146.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT6-0014-0008
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