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  • STRUCTURAL MECHANICS  (22)
  • Humans  (13)
  • 2015-2019  (13)
  • 1970-1974  (22)
  • 1935-1939
  • 1
    Publication Date: 2015-10-17
    Description: Human skin relies on cutaneous receptors that output digital signals for tactile sensing in which the intensity of stimulation is converted to a series of voltage pulses. We present a power-efficient skin-inspired mechanoreceptor with a flexible organic transistor circuit that transduces pressure into digital frequency signals directly. The output frequency ranges between 0 and 200 hertz, with a sublinear response to increasing force stimuli that mimics slow-adapting skin mechanoreceptors. The output of the sensors was further used to stimulate optogenetically engineered mouse somatosensory neurons of mouse cortex in vitro, achieving stimulated pulses in accordance with pressure levels. This work represents a step toward the design and use of large-area organic electronic skins with neural-integrated touch feedback for replacement limbs.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Tee, Benjamin C-K -- Chortos, Alex -- Berndt, Andre -- Nguyen, Amanda Kim -- Tom, Ariane -- McGuire, Allister -- Lin, Ziliang Carter -- Tien, Kevin -- Bae, Won-Gyu -- Wang, Huiliang -- Mei, Ping -- Chou, Ho-Hsiu -- Cui, Bianxiao -- Deisseroth, Karl -- Ng, Tse Nga -- Bao, Zhenan -- New York, N.Y. -- Science. 2015 Oct 16;350(6258):313-6. doi: 10.1126/science.aaa9306.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Department of Electrical Engineering, Stanford University, Stanford, CA, USA. ; Department of Materials Science and Engineering, Stanford University, Stanford, CA, USA. ; Department of Bioengineering, Stanford University, Stanford, CA, USA. ; Department of Chemistry, Stanford University, Stanford, CA, USA. ; Department of Chemical Engineering, Stanford University, Stanford, CA, USA. ; Xerox Palo Alto Research Center, Palo Alto, CA, USA. ; Department of Chemical Engineering, Stanford University, Stanford, CA, USA. zbao@stanford.edu.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/26472906" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Cerebral Cortex/cytology/physiology ; Hand/anatomy & histology/innervation/physiology ; Humans ; In Vitro Techniques ; *Mechanoreceptors ; Mice ; *Neural Prostheses ; Optogenetics ; Pressure ; Skin/*innervation ; *Touch ; Transcutaneous Electric Nerve Stimulation/*methods ; Transistors, Electronic
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 2
    Publication Date: 2016-06-07
    Description: A method is presented for obtaining the mass, stiffness, and damping parameters of a linear mathematical model, having fewer degrees of freedom than the structure it represents, directly from dynamic response measurements on the actual helicopter without a priori knowledge of the physical characteristics of the fuselage. The only input information required in the formulation is the approximate natural frequency of each mode and mobility data measured proximate to these frequencies with sinusoidal force excitation applied at only one point on the vehicle. The practicality and numerical soundness of the theoretical development was demonstrated through a computer simulation of an experimental program.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Ames Res. Center Rotorcraft Dyn.; p 239-248
    Format: application/pdf
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  • 3
    Publication Date: 2016-06-07
    Description: Antiresonance theory is the principle underlying nonresonant nodes in a structure, and covers both nonresonant nodes occurring naturally and those introduced by devices such as dynamic absorbers and antiresonant isolators. The dynamic antiresonant vibration isolator (DAVI) and the nodale module are examples of the applications of transfer antiresonances. It is shown that antiresonances are eigenvalues, and that they can be determined by matrix iteration. Applications of antiresonance theory to helicopter engineering problems, using the antiresonant eigenvalue equation are suggested.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Ames Res. Center Rotorcraft Dyn.; p 101-106
    Format: application/pdf
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  • 4
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    In:  CASI
    Publication Date: 2019-06-27
    Description: Research projects concerned with developing a theory of fracture of materials are discussed. The effects of the geometry of the structure and the loads acting on the structure as they influence the failure process are analyzed. The effects of the viscoelastic deformation characteristics of the bulk elastomer on failure behavior are examined. Additional material parameters which control the fracture process are identified.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-138125 , GALCIT-120
    Format: application/pdf
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  • 5
    Publication Date: 2019-06-27
    Description: The axisymmetric problem of a line load acting along the axis of a semiinfinite elastic solid is solved using Hankel transforms. In this solution the line load is interpreted as a body force loading and by assuming the line load to be of the form of a Dirac delta function the solution of Mindlin's problem of a point load within the interior of the half space is obtained. Solutions of this problem presented in the literature have been obtained using semiinverse techniques whereas the solution given here is obtained in a systematic step-by-step manner.
    Keywords: STRUCTURAL MECHANICS
    Type: ASME PAPER 71-APMW-1
    Format: text
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  • 6
    facet.materialart.
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    In:  Other Sources
    Publication Date: 2019-06-27
    Description: Crack propagation model in linearly viscoelastic solid strip based on thermodynamics first law
    Keywords: STRUCTURAL MECHANICS
    Type: ; - DISCRETE CONTROL S
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  • 7
    Publication Date: 2019-06-27
    Description: Fracture mechanics and time dependent strength of elastic or viscoelastic solids adhesively jointed by soft polymeric bonding layer
    Keywords: STRUCTURAL MECHANICS
    Type: ; ADEMIE DES SCIENCES
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  • 8
    Publication Date: 2019-06-27
    Description: Design data for regeneratively cooled panels from low cycle fatigue evaluation of Hastelloy X and Inconel 625 sheet and sandwich panel specimens
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-1884 , REPT-68-4313
    Format: application/pdf
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  • 9
    Publication Date: 2019-06-27
    Description: Incomplete models of dynamic structures
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-109630 , R-826
    Format: application/pdf
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  • 10
    Publication Date: 2019-07-13
    Description: Limited frequency range analytical model for predicting mass and stiffness changes effect on natural frequencies and normal modes
    Keywords: STRUCTURAL MECHANICS
    Type: MATERIALS AND STRUCTURAL DYNAMICS, AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS AND AMERICAN SOCIETY OF MECHANICAL ENGINEERS, STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE, 11TH; Apr 22, 1970 - Apr 24, 1970; DENVER, CO
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