Mechanical Engineering Exam > Mechanical Engineering Tests > Fluid Mechanics for Mechanical Engineering > Test: Flow of Compressible Fluids - 2 - Mechanical Engineering MCQ
Test: Flow of Compressible Fluids - 2 - Mechanical Engineering MCQ
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10 Questions MCQ Test Fluid Mechanics for Mechanical Engineering - Test: Flow of Compressible Fluids - 2
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Detailed Solution for Test: Flow of Compressible Fluids - 2 - Question 2
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Test: Flow of Compressible Fluids - 2 - Question 3
Consider the curves in the sketch shown below 
indicates normal shock)
Out of these curves, those which are not correctly drawn will include
indicates normal shock)Out of these curves, those which are not correctly drawn will include
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Test: Flow of Compressible Fluids - 2 - Question 4
Consider the following statements:
A tube, with the section diverging in the direction of flow, can be used as
1. Supersonic nozzle
2. Subsonic nozzle
3. Supersonic diffuser
4. Subsonic diffuser
Select the correct answer using the codes given below:
Detailed Solution for Test: Flow of Compressible Fluids - 2 - Question 4
Test: Flow of Compressible Fluids - 2 - Question 5
Match List-I with List-ll and select the correct answer using the codes given below the lists:
Test: Flow of Compressible Fluids - 2 - Question 6
An aeroplane is cruising at a speed of 800 kmph at an altitude, where the air temperature is 0°C. The flight Mach number at this speed is nearly,
Detailed Solution for Test: Flow of Compressible Fluids - 2 - Question 6
Test: Flow of Compressible Fluids - 2 - Question 8
Which one of the following properties drops across a normal shock?
Test: Flow of Compressible Fluids - 2 - Question 9
The flight Mach number of an aircraft flying at an altitude where the temperature is -48°C is 0.7. The speed of the aircraft is (Take γ = 1.4, 77= 287 J/kgK)
Test: Flow of Compressible Fluids - 2 - Question 10
What is the speed of sound in Neon gas at temperature of 500 K (Gas constant of Neon is 0.4210 kJ/kgK)?
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