Airport Engineering Total correction for elevation, temperature and gradient for a runway should not be more than 0.25 0.15 0.2 0.35 0.25 0.15 0.2 0.35 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the true speed of the aircraft and the crosswind component Between the horizontal and the fuselage axis Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the true speed of the aircraft and the crosswind component ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Speed of Sound at 0°C is called one Mach Sound varies 2.4 kmph per degree centigrade rise in temperature All listed here Sound at 0°C is 1190 kmph Sound at 0°C is called one Mach Sound varies 2.4 kmph per degree centigrade rise in temperature All listed here Sound at 0°C is 1190 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The depressions and undulations in the pavement, are caused due to Punching effect Improper compaction of sub-grade All listed here Impact of heavy wheel loads Punching effect Improper compaction of sub-grade All listed here Impact of heavy wheel loads ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the transitional surface for A, B and C type of runway shall be 0.046527777777778 0.05 0.048611111111111 0.045138888888889 0.046527777777778 0.05 0.048611111111111 0.045138888888889 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The air is blowing at a speed of 75 knots in the direction of the aircraft flying at a ground speed of 775 knots. The air speed of the aircraft, is 75 knots 775 knots 675 knots 850 knots 75 knots 775 knots 675 knots 850 knots ANSWER DOWNLOAD EXAMIANS APP
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