82 pages matching editions:ISBN0471324809 in this book
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AN APPROACH TO RELIABILITY
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achieved performance aircraft alternating renewal process apply aspects assumptions basic requirement Boolean circuit coefficient combined complete component confidence limits connexion considered constant corresponding cumulative distribution function cumulative probability defined dependent derived described diagram discrete electrical electronic amplifier estimate evaluation Example exponential distribution expressed failed faults given in Equation hazard function Hence input conditions input function instance interval Laplace transform large number logical lower limit matrix mean availability mean failure-rate mean fractional dead mean number mean value method nominally identical non-redundant system normal distribution number of failures obtained occur operation output conditions output function parent population period Poisson Poisson distribution probability density function random variations range rectangular distribution relevant repair represents required performance resistor sample means shown in Figure similar standard deviation standby successful system failure Table technological system total number transfer function truth table upper limit variable variance voltage zero