These tools will no longer be maintained as of December 31, 2024. Archived website can be found here. PubMed4Hh GitHub repository can be found here. Contact NLM Customer Service if you have questions.


BIOMARKERS

Molecular Biopsy of Human Tumors

- a resource for Precision Medicine *

124 related articles for article (PubMed ID: 37444903)

  • 1. Effect of Mechanical Heterogeneity on the Structural Integrity of HTPB Propellant Grain.
    Liu X; Hui B; Wang H; Chen H; Zhou D
    Materials (Basel); 2023 Jun; 16(13):. PubMed ID: 37444903
    [TBL] [Abstract][Full Text] [Related]  

  • 2. Dynamic Mechanical Response and Damage Mechanism of HTPB Propellant under Impact Loading.
    Zhang H; Liu M; Miao Y; Wang H; Chen T; Fan X; Chang H
    Materials (Basel); 2020 Jul; 13(13):. PubMed ID: 32645902
    [TBL] [Abstract][Full Text] [Related]  

  • 3. Structural Integrity Assessment of an NEPE Propellant Grain Considering the Tension-Compression Asymmetry in Its Mechanical Property.
    Zhang P; Han W; Zhou D; Wu H
    Polymers (Basel); 2023 Aug; 15(16):. PubMed ID: 37631396
    [TBL] [Abstract][Full Text] [Related]  

  • 4. Study on Mechanical Properties and Failure Mechanisms of Highly Filled Hydroxy-Terminated Polybutadiene Propellant under Different Tensile Loading Conditions.
    Wu C; Lu Y; Jiang M; Hu S; Yang H; Fu X; Li H
    Polymers (Basel); 2023 Sep; 15(19):. PubMed ID: 37835918
    [TBL] [Abstract][Full Text] [Related]  

  • 5. Numerical Conversion Method for the Dynamic Storage Modulus and Relaxation Modulus of Hydroxy-Terminated Polybutadiene (HTPB) Propellants.
    Ji Y; Cao L; Li Z; Chen G; Cao P; Liu T
    Polymers (Basel); 2022 Dec; 15(1):. PubMed ID: 36616352
    [TBL] [Abstract][Full Text] [Related]  

  • 6. A Nonlinear Viscoelastic Constitutive Model for Solid Propellant with Rate-Dependent Cumulative Damage.
    Chen S; Wang C; Zhang K; Lu X; Li Q
    Materials (Basel); 2022 Aug; 15(17):. PubMed ID: 36079214
    [TBL] [Abstract][Full Text] [Related]  

  • 7. Numerical Analysis of Curing Residual Stress and Strain in NEPE Propellant Grain.
    Liu X; Xie X; Zhou D; Wang R
    Polymers (Basel); 2023 Feb; 15(4):. PubMed ID: 36850301
    [TBL] [Abstract][Full Text] [Related]  

  • 8. Biaxial tensile test and meso damage numerical simulation of HTPB propellant.
    Wang Q; Wang G; Wang Z; Qiang H; Wang X; Li S; Zhu Z
    Sci Rep; 2022 Oct; 12(1):17635. PubMed ID: 36271139
    [TBL] [Abstract][Full Text] [Related]  

  • 9. Establishment of a NIR-based methodology for tracking the blend homogeneity of HTPB propellant slurry in the mixing process.
    Wang W; Xie L; Wang Z; Deng G
    Spectrochim Acta A Mol Biomol Spectrosc; 2023 Jan; 285():121869. PubMed ID: 36116411
    [TBL] [Abstract][Full Text] [Related]  

  • 10. Influence of Thermally-Accelerated Aging on the Dynamic Mechanical Properties of HTPB Coating and Crosslinking Density-Modified Model for the Payne Effect.
    Du Y; Zheng J; Yu G
    Polymers (Basel); 2020 Feb; 12(2):. PubMed ID: 32053946
    [TBL] [Abstract][Full Text] [Related]  

  • 11. Effect of Microstructure on Micro-Mechanical Properties of Composite Solid Propellant.
    Li T; Xu J; Han J; He Y
    Micromachines (Basel); 2021 Nov; 12(11):. PubMed ID: 34832790
    [TBL] [Abstract][Full Text] [Related]  

  • 12. Comparative Study on Thermal Response Mechanism of Two Binders during Slow Cook-Off.
    Wu X; Li J; Ren H; Jiao Q
    Polymers (Basel); 2022 Sep; 14(17):. PubMed ID: 36080774
    [TBL] [Abstract][Full Text] [Related]  

  • 13. Review of novel energetic polymers and binders - high energy propellant ingredients for the new space race.
    Cheng T
    Des Monomers Polym; 2019; 22(1):54-65. PubMed ID: 30863243
    [TBL] [Abstract][Full Text] [Related]  

  • 14. Hyperbranched polyamide modified graphene oxide-reinforced polyurethane nanocomposites with enhanced mechanical properties.
    Liu Y; Zheng J; Zhang X; Du Y; Yu G; Li K; Jia Y; Zhang Y
    RSC Adv; 2021 Apr; 11(24):14484-14494. PubMed ID: 35424010
    [TBL] [Abstract][Full Text] [Related]  

  • 15. Experimental and Numerical Investigation into the Mechanical Behavior of Composite Solid Propellants Subject to Uniaxial Tension.
    Wu C; Jiang M; Lu Y; Qu H; Li H; Hu S
    Materials (Basel); 2023 Oct; 16(20):. PubMed ID: 37895677
    [TBL] [Abstract][Full Text] [Related]  

  • 16. AP-HTPB propellant combustion under strain conditions with laser absorption spectroscopy.
    Gu M; Ouyang J; Wang S; Yuan W; Shi X; Hou K; Xiao L; Gao H; Zhou Z; Qi F
    Appl Opt; 2023 Feb; 62(6):A37-A45. PubMed ID: 36821298
    [TBL] [Abstract][Full Text] [Related]  

  • 17. A Viscometric study of mixtures with Hydroxyl-terminated polybutadiene (HTPB) and short chain diols used in the formulations of solid composite propellants.
    Cunha BCCD; Domingues MG; Rocco JAFF
    An Acad Bras Cienc; 2021; 93(suppl 4):e20201729. PubMed ID: 34706006
    [TBL] [Abstract][Full Text] [Related]  

  • 18. Performance and Kinetics Study of Self-Repairing Hydroxyl-Terminated Polybutadiene Binders Based on the Diels⁻Alder Reaction.
    Liang C; Li J; Xia M; Li G; Luo Y
    Polymers (Basel); 2017 May; 9(6):. PubMed ID: 30970877
    [TBL] [Abstract][Full Text] [Related]  

  • 19. First applications of ultrasound technology in solid rocket propellant combustion promotion.
    Wen Z; Jing H; Hao F; Wang Y; Kuang B; Liu P; Ao W
    Ultrason Sonochem; 2024 Oct; 111():107107. PubMed ID: 39418767
    [TBL] [Abstract][Full Text] [Related]  

  • 20. A nonlinear viscoelastic constitutive model with damage and experimental validation for composite solid propellant.
    Li H; Xu JS; Chen X; Zhang JF; Li J
    Sci Rep; 2023 Feb; 13(1):2049. PubMed ID: 36739301
    [TBL] [Abstract][Full Text] [Related]  

    [Next]    [New Search]
    of 7.