A Viscoelastic Constitutive Model of Composite Propellant Considering Dewetting and Strain‐Rate and its Implementation
Author:
Affiliation:
1. College of Aerospace Science and EngineeringNational University of Defence Technology 410073 Changsha P.R. China
2. Institute for Turbomachinery and Flight PropulsionTechnical University of Munich 85748 Garching b. München Germany
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201800264
Reference23 articles.
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2. Z. J. Wang H. F. Qiang G. Wang Q. Z. Huang Tensile mechanical properties and constitutive model for HTPB propellant at low temperature and high strain rate J. Appl. Polym. Sci.2015 132.
3. X. D. Chen X. L. Chang Y. H. Zhang B. Wang Q. Zhang X. Zhang Tensile Mechanical Properties of HTPB Propellant at Low Temperature Key Eng. Mater.2018 765 54–59.
4. C. Erişken A. Göçmez Ü. Yilmazer F. Pekel S. Özkar Modeling and rheology of HTPB based composite solid propellants Polym. Compos.2010 19 463–472.
5. S. Y. Ho High Strain-Rate Constitutive Models for Solid Rocket Propellants J. Propul. Power2002 18 1106–1111.
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