Li, Y.; Xu, J.; Zhou, C.; Chen, X.; Yang, X.
Constitutive Model Based on Stress Relaxation for Composite Modified Double-Base Propellants and Master Curve of Relaxation Modulus. Aerospace 2025, 12, 817.
https://doi.org/10.3390/aerospace12090817
AMA Style
Li Y, Xu J, Zhou C, Chen X, Yang X.
Constitutive Model Based on Stress Relaxation for Composite Modified Double-Base Propellants and Master Curve of Relaxation Modulus. Aerospace. 2025; 12(9):817.
https://doi.org/10.3390/aerospace12090817
Chicago/Turabian Style
Li, Yao, Jinsheng Xu, Changsheng Zhou, Xiong Chen, and Xiumin Yang.
2025. "Constitutive Model Based on Stress Relaxation for Composite Modified Double-Base Propellants and Master Curve of Relaxation Modulus" Aerospace 12, no. 9: 817.
https://doi.org/10.3390/aerospace12090817
APA Style
Li, Y., Xu, J., Zhou, C., Chen, X., & Yang, X.
(2025). Constitutive Model Based on Stress Relaxation for Composite Modified Double-Base Propellants and Master Curve of Relaxation Modulus. Aerospace, 12(9), 817.
https://doi.org/10.3390/aerospace12090817