Aerospace Engineering > GATE 2026 > Takeoff Performance
WA and WB are the respective maximum take-off weights of an aircraft for two ambient air conditions given below.
Condition A: p = 1 bar, T = 50 °C; Condition B: p = 0.66 bar, T = −30 °C
If all other parameters relevant for take-off are kept the same in these two conditions, the ratio WB/WA is ________ (rounded off to 3 decimal places).

Correct : 0.905

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