Ask
Login
TAGGED IN

Fluid Mechanics

Follow this tag to get notifications whenever a new post is added

ALL TAGS
2
votes
1
answer
6.1k
views
1
answer
A siphon of diameter 200mm connects two reservoirs having a difference in elevation of 15m. The total length of siphon is 600 m and the summit is 4 m above the water level in the upper reservoir.
fluid mechanics updated 18 months ago by Chandan15 • 300
3
votes
1
answer
17k
views
1
answer
Write a short note on Moodys Diagram
fluid mechanics updated 23 months ago by anushkazod936 • 30
1
vote
1
answer
782
views
1
answer
Write short note on aerofoil theory
fluid mechanics updated 24 months ago by Krishna_Agrawal • 2.6k
0
votes
1
answer
745
views
1
answer
Classify lubricating oil using viscosity (SAE) and load severity (API) rating.
fluid mechanics updated 24 months ago by pedsangini276 • 4.7k
1
vote
1
answer
8.2k
views
1
answer
The velocity components in two dimensional flow field are as follows 10
fluid mechanics updated 24 months ago by safahameedmaj152 • 20
2
votes
1
answer
802
views
1
answer
Write short note on Minor losses in pipe.
fluid mechanics updated 24 months ago by DevarenjiniP • 3.1k
0
votes
1
answer
724
views
1
answer
Explain a Sonic Velocity for Isothermal Process and Adiabatic Process.
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
3
votes
1
answer
838
views
1
answer
What is Shock waves? explain about Normal Shock Wave.
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
0
votes
0
answers
615
views
0
answers
(Duplicate) take mass density of air $1.205 kg/m^3$ , CD =1.33.
fluid mechanics updated 24 months ago by sagarkolekar ★ 11k
3
votes
1
answer
3.0k
views
1
answer
Hydraulic jump Numerical
fluid mechanics updated 24 months ago by RakeshBhuse • 3.2k
2
votes
1
answer
2.7k
views
1
answer
Determine the viscosity of the oil.
fluid mechanics updated 24 months ago by Krishna_Agrawal • 2.6k
0
votes
1
answer
1.7k
views
1
answer
At some section in the convergent-divergent nozzle, in which air is flowing, pressure, velocity, temperature and cross-sectional area are 200,,,
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
2
votes
1
answer
610
views
1
answer
Assuming adiabatic flow, find the mass rate of flow of air through the nozzle to the atmosphere when the pressure in the tank is,
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
0
votes
1
answer
946
views
1
answer
For a normal shock wave in air Mach number is 2. If the atmospheric pressure and air density are 26.5 kN/m2 and 0.413 kg/m3 respectively, determine the flow conditions before and after the shock wave.
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
1
vote
1
answer
1.1k
views
1
answer
For the velocity profile for laminar boundary flow
fluid mechanics updated 24 months ago by RakeshBhuse • 3.2k
0
votes
1
answer
2.4k
views
1
answer
Fluid is in laminar motion between two parallel plates separated by distance b under the action of motion of one of the plates and also under the presence of a pressure
fluid mechanics updated 24 months ago by RakeshBhuse • 3.2k
0
votes
1
answer
3.0k
views
1
answer
Compressible Fluid Flow
fluid mechanics updated 24 months ago by RakeshBhuse • 3.2k
0
votes
1
answer
775
views
1
answer
Boundary Layer Flows
fluid mechanics updated 24 months ago by RakeshBhuse • 3.2k
2
votes
1
answer
568
views
1
answer
Explain the Laval nozzle (convergent-divergent nozzle).
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
2
votes
1
answer
390
views
1
answer
Determine the reservoir pressure, temperature and the throat area. Take $\gamma=1.4$.
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
0
votes
1
answer
299
views
1
answer
Air at a pressure of $220 \mathrm{kN} / \mathrm{m}^{2}$ and temperature $27^{\circ} \mathrm{C}$ is moving at a velocity of $200 \mathrm{~m} / \mathrm{s}$. Calculate the stagnation pressure if,
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
0
votes
1
answer
316
views
1
answer
The gauge indicates a velocity of $152 m/s$. What is the true speed of the aircraft ?
fluid mechanics updated 24 months ago by prajapatijaimin • 3.1k
0
votes
1
answer
1.8k
views
1
answer
Calculate on the stagnation point on the nose of the plane.
fluid mechanics updated 2.0 years ago by prajapatijaimin • 3.1k
0
votes
1
answer
1.5k
views
1
answer
Compute its stagnation properties and the local Mach number.
fluid mechanics updated 2.0 years ago by prajapatijaimin • 3.1k
0
votes
1
answer
765
views
1
answer
The velocity profile within a laminar boundary layer over a flat plate is given by the equation
fluid mechanics updated 2.0 years ago by RakeshBhuse • 3.2k
<prev • 184 results • page 1 of 8 • next >