Frequency table of usefulness of three-dimensional printed heart models in communication in medical practice.

Frequency table of usefulness of three-dimensional printed heart models in medical education.

This table shows participant comparative physiology open-ended definitions word frequency

This table is part of a series of tables that present a portrait of Canada based on the various census topics. The tables range in complexity and levels of geography. Content varies from a simple overview of the country to complex cross-tabulations; the tables may also cover several censuses.

Figure 1. Electrosurgical cutting experimental setup and electrode sample, (a) Electrosurgical cutting experimental setup,1-ESU, 2-feeding device, 3-active electrode pen, 4-active electrode, 5-porcine liver, 6-dispersive electrode, 7-locating device; (b) Standard blade-type 304 stainless steel monopolar active electrode Figure 2. Schematic diagrams of heat-adherence test and thermographs, (a) Schema of heat-adherence test; (b) Thermograph of heat-adherence test, side view; (c) Thermograph of heat-adherence test, front view; (d) Thermograph of electrosurgical cutting Figure 3. Schematic representation of tensile test samples’ preparation Figure 4. SEM micrographs and EDX spectrums of electrode surfaces, (a) SEM micrograph of original electrode; (b) EDX spectrum of original electrode; (c) SEM micrograph after electrosurgical cutting test; (d) EDX spectrum after electrosurgical cutting test; (e) SEM micrograph after heat-adherence test; (f) EDX spectrum after heat-adherence test Figure 5. FTIR spectrums of sticking tissues on electrode surfaces after the two tests Figure 6. SEM micrographs of electrode cross sections, (a) after electrosurgical cutting test; (b) after heat-adherence test Figure 7. Three-dimensional morphologies of cleaned surfaces of electrodes, (a) original electrode; (b) after electrosurgical cutting test; (c) after heat-adherence test Figure 8. OM micrographs of electrode surfaces after tensile testing, (a) original electrode as a control; (b) electrode from heat-adherence test; (c) electrode from electrosurgical cutting test. Figure 9. Histological examples of porcine liver tissue sample after electrosurgical cutting test Figure 10. SEM micrograph and EDX spectrum of the electrode surface after smoke collection, (a) SEM micrograph; EDX spectrum Figure 11. Schematic diagrams of porcine liver tissue, electrosurgery procedure and formation process of sticking tissue upon electrode, (a) porcine liver tissue; (b) electrosurgery procedure; (c) formation process of sticking tissue upon electrode;Tensile properties of sticking tissue-electrode interface after electrosurgical cutting test and heat-adherence test

On Board Fast Fourier Transform (FFT) power spectra of Electric (EFI) and Magnetic (SCM) field measurements for particle and wave burst survey modes. Spectra are produced only in Particle Burst and Wave Burst modes; only a preselected four of the signals listed in Table 1 are input at any time. Data fed through the FFT while not in Particle or Wave Burst modes is automatically disgarded. The FFTs (Cooley-Tukey algorithm) are conducted as an integral part of the power spectrum calculation by the Field Programable Gate Arrays (FPGAs). A CORDIC algorithm is used for sine/cosine calculations. The data has raw resolution of 1024 pts for 8,192 sample/sec signals and 2048 pts for 16,384 sample/sec signals (EAC measurements only). Signals at 8,192 samples/sec are handled by 1024-point FFTs, while those at 16,384 samples/sec go through 2048-point FFTs. Past and current signal configurations for specific spacecraft are listed bellow in Table 2. The spectra are arranged into log spaced frequency bins in steps of 16, 32, or 64. Cadence is adjusted to keep packet size constant (i.e. increasing the fequency resolution by a factor of 2 decreases the sampling rate by 1/2). The frequency bins cover a range of 0 Hz to 4 kHz. Table 1: FFT Input Signals. Signal Description SCMX, SCMY, SCMZ: Three axis magnetic fiend from SCM V1 through V6: Probe-spacecraft voltage for all six EFI sensors E12DC, E34DC, E56DC: DC-coupled electric field measured from opposing EFI sensors E12AC, E34AV, E56AC: AC-coupled electric field measured from opposing EFI sensors E12HF: High frequency electric field from EFI Table 2: Spacecraft specific configurations. All probes were initially set to use EDC34, EDC56, SCM2, and SCM3 signals for both particle and wave burst modes. Output was set to 16 frequency bins at 4 Hz. Configuration Changes: 23-27 June 2008: Particle burst spectra on all probes reconfigured to 64 bins at 1 Hz. Table 3: Instrument-Spacecraft Physical Configuration Instrument Alignment in Spacecraft Geometric coordinates (SPG). See THEMIS website for coordinate system details and mechanical drawings. EFI boom 1: Along positive X-axis EFI boom 2: Along negative X-axis EFI boom 3: Along positive Y-axis EFI boom 4: Along negative Y-axis EFI boom 5: Along positive Z-axis EFI boom 6: Along negative Z-axis SCM *The SCM uses an instrument specific set of axes; an orthogonal system centered instrument with the X-axis 12.1 degrees from the SPG X-axis.