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THE X DISTRIBUTION
APPLICATIONS TO REAL DATA
3 other sections not shown
additions airplane alleviation alloys angle annealing Apollo assembly basic blankets Block calculated Center changes characteristics chi-square components conducted considered Continued correlation determined deviations dimensions discussed distribution effects equation failure Figure film flame flap flight frequency friction function gravity gyro heat increased indicated input insulation lift load located material mean measured median memory metal meter module multivariate NASA normal observed obtained operation percent Percentile performance pitching points position presented pressure Probability problem radiation random ratio reduced reference response Runs sample selected shown shows sliding Space square static Statistics surface TABLE tank temperature term thermal toughness transfer units values vane variate wall wear zero