Publication | Closed Access
Compressive mechanical properties of HTPB propellant at low, intermediate, and high strain rates
43
Citations
38
References
2016
Year
EngineeringProfile ModificationMechanical EngineeringMechanics ModelingFluid PropertiesUniversal Testing MachineMechanicsCompression (Physics)Stressstrain AnalysisHigh Strain RatesHtpb PropellantMaterials ScienceCompressive Mechanical PropertiesSolid MechanicsMaterial MechanicsMechanical PropertiesConstitutive ModelingAbstract LowMechanics Of MaterialsHigh Strain Rate
ABSTRACT Low, intermediate, and high strain rate compression testing (1.7 × 10 −4 to 2500 s −1 ) of the hydroxyl‐terminated polybutadiene (HTPB) propellant at room temperature, were performed using a universal testing machine, a hydraulic testing machine, and a split Hopkinson pressure bar (SHPB), respectively. Results show that the stress linearly increases with strain at each condition; the increasing trend of stress at a given strain with the logarithm of strain rate changes from a linear to an exponential form at 1 s −1 . By combining these characteristics, we propose a rate‐dependent constitutive model which is a linearly elastic component as a base model, then multiplied by a rate‐dependent component. Comparison of model with experimental data shows that it can characterize the compressive mechanical properties of HTPB propellant at strain rates from 1.7 × 10 −4 to 2500 s −1 . © 2016 Wiley Periodicals, Inc. J. Appl. Polym. Sci. 2016 , 133 , 43512.
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