Civil Engineering - UPSC Civil Service Exam Questions
Exercise : UPSC Civil Service Exam Questions - Section 21
- UPSC Civil Service Exam Questions - Section 14
- UPSC Civil Service Exam Questions - Section 27
- UPSC Civil Service Exam Questions - Section 26
- UPSC Civil Service Exam Questions - Section 25
- UPSC Civil Service Exam Questions - Section 24
- UPSC Civil Service Exam Questions - Section 23
- UPSC Civil Service Exam Questions - Section 22
- UPSC Civil Service Exam Questions - Section 21
- UPSC Civil Service Exam Questions - Section 20
- UPSC Civil Service Exam Questions - Section 19
- UPSC Civil Service Exam Questions - Section 18
- UPSC Civil Service Exam Questions - Section 17
- UPSC Civil Service Exam Questions - Section 16
- UPSC Civil Service Exam Questions - Section 15
- UPSC Civil Service Exam Questions - Section 1
- UPSC Civil Service Exam Questions - Section 13
- UPSC Civil Service Exam Questions - Section 12
- UPSC Civil Service Exam Questions - Section 11
- UPSC Civil Service Exam Questions - Section 10
- UPSC Civil Service Exam Questions - Section 9
- UPSC Civil Service Exam Questions - Section 8
- UPSC Civil Service Exam Questions - Section 7
- UPSC Civil Service Exam Questions - Section 6
- UPSC Civil Service Exam Questions - Section 5
- UPSC Civil Service Exam Questions - Section 4
- UPSC Civil Service Exam Questions - Section 3
- UPSC Civil Service Exam Questions - Section 2
16.
The coordinates of two end-points A and B traverse line AB are XA = 1000.00 m, YA = 1000.00 m XB = 2000.00 m, YB = 1000.00 m The bearing of the line AB will be
17.
Consider the following statements relating to compressible flow :
1. In a contracting conduit, sonic velocity is reached in the minimum cross-sectional area.
2. In a contracting conduit, supersonic velocities are reached only in the expanding section downstream from the minimum section.
3. An expansion shockwave is physically possible and can be exhibited.
4. In the Laval nozzle it is possible to obtain a velocity greater than the velocity of sound in the expanding section of nozzle.
Of these statements :
1. In a contracting conduit, sonic velocity is reached in the minimum cross-sectional area.
2. In a contracting conduit, supersonic velocities are reached only in the expanding section downstream from the minimum section.
3. An expansion shockwave is physically possible and can be exhibited.
4. In the Laval nozzle it is possible to obtain a velocity greater than the velocity of sound in the expanding section of nozzle.
Of these statements :
18.
Consider the following factors :
1. Elevation
2. Temperature
3. Gradient
4. Trip length.
For finding the runway length, which of these are taken into reckoning ?
1. Elevation
2. Temperature
3. Gradient
4. Trip length.
For finding the runway length, which of these are taken into reckoning ?
19.
Which one of the following is the reaction of the cantilever at B as shown in the figure ?


20.
If a road surface is adequately superelevated on horizontal curve, which one of the following is the proper distribution of pressure on the vehicle wheels ?
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