In this problem, we are given two engines, each with reliability \( R \), and the aircraft will only crash if both engines fail. This implies that the aircraft will not crash as long as at least one engine is working. To find the reliability of the aircraft flying without crashing, we first need to calculate the probability of both engines failing, as the complement of this will give us the desired reliability.
The probability of one engine failing is \( 1 - R \), and the probability that both engines fail (i.e., both engines stop working) is: \[ (1 - R)^2 \] Therefore, the probability that at least one engine is working (i.e., the aircraft does not crash) is the complement of this probability: \[ 1 - (1 - R)^2 \] Expanding this expression: \[ 1 - (1 - 2R + R^2) = 2R - R^2 \] Thus, the reliability of the aircraft flying without crashing is \( 2R - R^2 \), which corresponds to option (C).
A through hole of 10 mm diameter is to be drilled in a mild steel plate of 30 mm thickness. The selected spindle speed and feed for drilling hole are 600 revolutions per minute (RPM) and 0.3 mm/rev, respectively. Take initial approach and breakthrough distances as 3 mm each. The total time (in minute) for drilling one hole is ______. (Rounded off to two decimal places)
In a cold rolling process without front and back tensions, the required minimum coefficient of friction is 0.04. Assume large rolls. If the draft is doubled and roll diameters are halved, then the required minimum coefficient of friction is ___________. (Rounded off to two decimal places)