Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Pick up the component not applicable to aeroplanes Wings Engines None of these Air screw Wings Engines None of these Air screw ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering According to I.C.A.O. the recommended length of air ports is decided on Effective gradient percentage Sea level elevation All listed here Standard sea level temperature (15°C) Effective gradient percentage Sea level elevation All listed here Standard sea level temperature (15°C) ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Mach Super-sonic Subsonic Sonic Mach Super-sonic Subsonic Sonic ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The minimum width of clearway is 150 m 50 m 250 m 100 m 150 m 50 m 250 m 100 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The engine failure case for determining the basic runway length may require Only clearway Either a clearway or a stop-way or both Either a clearway or a stop-way Only stop way Only clearway Either a clearway or a stop-way or both Either a clearway or a stop-way Only stop way ANSWER DOWNLOAD EXAMIANS APP
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