self-induced การใช้

• A paradox of the self - induced coefficient of solid cable
• A self - induced hypnotic state
• The analysis of self - induced emf in rl circuit and its experimental design
• Self - excited or self - induce vibrations
• Self - induced vibration
• An analysis of factors that impact maximum self - induced emf in open rl circuit
• In the near field , the vortex pairs are gradually and periodically formed , and at the same time they migrate down stream under the self - induced velocity
• Its peculiarity is that the vortex pair formed on the ejection stroke can ? move far enough under the self - induced velocity , so the vortex pair is sucked into the cavity of the actuator during the suction stroke
• An eating disorder in which one alternates between abnormal craving for and aversion to food . it is characterized by episodes of excessive food intake followed by periods of fasting and self - induced vomiting or diarrhea
• The flying stability of the unguided projectile with wrap around fins could be influenced by the self - induced rolling characteristics and the cross coupling effects of the waf badly . it is necessary to study further on this special aerodynamic problems
• An attempt is made to explore self - induced emf in theory by a quantitative means , and to demonstrate the corresponding contents or its experimental design by using the instruments such as voltage effect and digital oscillograph
• Those who had prolonged binging and severely self - induced vomiting may have their stomach , eyes capillaries , internal mouthparts and fingers damaged , resulting in facial swelling or dental erosion . older age of onset and persistent fat - phobia were found to independently predict the poor outcome
• The influence of the blowing factors to the flutter and the lift coefficient is analyzed . secondly , the self - induced vibration of seals are analyzed by fluid - structure coupling numerical method . the self - induced oscillation of the seals will occur at large rotational speed , however , this phenomenon ca n ' t be simulated with the
• Firstly , the airfoil ' s classic flutter ( at small attack angle ) , stall flutter ( near the static stall angle ) and response ( at large attack angle ) are analyzed . it is found from the numerical results that " lock - in " will occur at certain freestream velocity range near the static stall angle , where the frequency of the vortex will be equal to the natural frequency and the flutter has the characteristic of self - induced oscillation . when the attack angle is far from the static stall angle , the vortex will have its own frequency , which differs from the natural frequency , and the flutter has the characteristic of forced oscillation