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Airport Engineering

Airport Engineering
For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is

0.5
0.75
0.4
0.6

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Airport Engineering
The slope of the transitional surface for A, B and C type of runway shall be

0.045138888888889
0.05
0.048611111111111
0.046527777777778

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Airport Engineering
International Civil Aviation Organization (I.C.A.O.) was set up at Montreal (Canada), in

1929
1947
1939
1950

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Airport Engineering
An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as

Mach
Sonic
Subsonic
Super-sonic

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Airport Engineering
The depressions and undulations in the pavement, are caused due to

Improper compaction of sub-grade
All listed here
Punching effect
Impact of heavy wheel loads

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Airport Engineering
The length of runway under standard conditions is 2000 m. The elevation of airport site is 300 m. Its reference temperature is 33.05°C. If the runway is to be constructed with an effective gradient of 0.25 percent, the corrected runway length will be

2600 m
2500 m
2700 m
2800 m

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