Analysis of uniaxial tensile tests for homogeneous solid propellants under various loading conditions

Central European Journal of Energetic Materials

Volumn 8, Issue 4, 2011, Pages 223-231

  Zalewski, Robert ^a   Wolszakiewicz, Tomasz ^b  

^a WARSAW UNIVERSITY OF TECHNOLOGY   (Poland)

^b INSTITUTE OF INDUSTRIAL ORGANIC CHEMISTRY   (Poland)

Author keywords

Experimental results; Solid propellants; Strain rate; Temperature

Indexed keywords

EID: 84859115399     PISSN: 17337178     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (6)

1. Jung G., Youn S., Kim B., A Three-Dimensional Nonlinear Viscoelastic Constitutive Model of Solid Propellant, Int. J. Solids Struct., 2000, 37, 4715-4732.
2. Rao S., Krishna Y., Rao B., Fracture Toughness of Nitramine and Composite Solid Propellants, Mat. Sci. Eng. A, 2005, 403, 125-133.
3. Renganathan K., Rao B., Jana M., Failure Pressure Estimations on Solid Propellant Rocket Motor with a Circular Perforated Grain, Int. J. Pres. Ves. Pip., 1999, 76, 955-963.
4. Pyrz M., Wolszakiewicz T., Zalewski R., Modeling of Solid Propellants Nonlinear Properties with Thermal Loading History, Machine Dynamics Problems, 2008, 32(3), 80-91.
5. Wolszakiewicz T., Zalewski R., Modelowanie zachowań stałych paliw rakietowych obcia{ogonek}żonych mechanicznie i termicznie, Naukowe Aspeky Uzbrojenia i Bezpieczeństwa, (Gacek J., Kostyrow R., Milewski E., Eds.), Wojskowa Akademia Techniczna, Warszawa 2008, pp. 141-151 (in Polish).
6. Zalewski R., Pyrz M., Wolszakiewicz T., Modeling of Solid Propellants Viscoplastic Behavior Using Evolutionary Algorithms, Cent. Eur. J. Energ. Mater., 2010, 7(4), 115-129.