• DocumentCode
    129384
  • Title

    Loading ramp effects in uniaxial compression creep device

  • Author

    Amador, Carolina ; Nabavizadeh, Alireza ; Kinnick, Randall ; Fatemi, Mehdi

  • Author_Institution
    Dept. of Physiol. & Biomed. Eng., Mayo Clinic Coll. of Med., Rochester, MN, USA
  • fYear
    2014
  • fDate
    3-6 Sept. 2014
  • Firstpage
    2320
  • Lastpage
    2322
  • Abstract
    Tissue viscoelastic properties measured by uniaxial compression creep ultrasound method have shown correlation with tissue state. The majority of creep studies assume step-loading conditions, which are analytically convenient but experimentally impossible to implement. The goals of the study were to compare global creep response using a conventional mechanical testing machine to a prototype compression device as well as studying the effects of loading rate in the creep response. A 10% gelatin phantom was tested with the prototype compression device and a commercial mechanical testing machine with a 3 N force held for 30 seconds and loading rates of 3 N/s and 20 N/s. Additionally a Dynamic Mechanical Analysis (DMA) was used to characterize the phantom viscoelastic properties. The measured loss tangent with prototype compression device and commercial mechanical testing machine were similar and converged to DMA results as the loading rate was increased.
  • Keywords
    bioacoustics; biological tissues; biomechanics; creep; phantoms; prototypes; viscoelasticity; Dynamic Mechanical Analysis; gelatin phantom; loading ramp effects; mechanical testing machine; prototype compression device; tissue viscoelastic property; ultrasound method; uniaxial compression creep device; Creep; Force; Loss measurement; Prototypes; Strain; Testing; Ultrasonic variables measurement; Uniaxial compression; creep; loading rate; tissue; viscoelasticity;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Ultrasonics Symposium (IUS), 2014 IEEE International
  • Conference_Location
    Chicago, IL
  • Type

    conf

  • DOI
    10.1109/ULTSYM.2014.0578
  • Filename
    6931931