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Fluid Mechanics

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2
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6.3k
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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 19 months ago by Chandan15 • 300
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Write a short note on Moodys Diagram
fluid mechanics updated 2.0 years ago by anushkazod936 • 30
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795
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Write short note on aerofoil theory
fluid mechanics updated 2.0 years ago by Krishna_Agrawal • 2.7k
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764
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Classify lubricating oil using viscosity (SAE) and load severity (API) rating.
fluid mechanics updated 2.0 years ago by pedsangini276 • 4.8k
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8.2k
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The velocity components in two dimensional flow field are as follows 10
fluid mechanics updated 2.0 years ago by safahameedmaj152 • 20
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815
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Write short note on Minor losses in pipe.
fluid mechanics updated 2.0 years ago by DevarenjiniP • 3.1k
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755
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Explain a Sonic Velocity for Isothermal Process and Adiabatic Process.
fluid mechanics updated 2.0 years ago by prajapatijaimin • 3.1k
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867
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What is Shock waves? explain about Normal Shock Wave.
fluid mechanics updated 2.0 years ago by prajapatijaimin • 3.1k
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(Duplicate) take mass density of air $1.205 kg/m^3$ , CD =1.33.
fluid mechanics updated 2.0 years ago by sagarkolekar ★ 11k
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3.1k
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Hydraulic jump Numerical
fluid mechanics updated 2.0 years ago by RakeshBhuse • 3.2k
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2.7k
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Determine the viscosity of the oil.
fluid mechanics updated 2.0 years ago by Krishna_Agrawal • 2.7k
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1.7k
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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 2.0 years ago by prajapatijaimin • 3.1k
2
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713
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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 2.1 years ago by prajapatijaimin • 3.1k
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992
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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 2.1 years ago by prajapatijaimin • 3.1k
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For the velocity profile for laminar boundary flow
fluid mechanics updated 2.1 years ago by RakeshBhuse • 3.2k
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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 2.1 years ago by RakeshBhuse • 3.2k
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3.0k
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Compressible Fluid Flow
fluid mechanics updated 2.1 years ago by RakeshBhuse • 3.2k
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Boundary Layer Flows
fluid mechanics updated 2.1 years ago by RakeshBhuse • 3.2k
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586
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Explain the Laval nozzle (convergent-divergent nozzle).
fluid mechanics updated 2.1 years ago by prajapatijaimin • 3.1k
2
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404
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Determine the reservoir pressure, temperature and the throat area. Take $\gamma=1.4$.
fluid mechanics updated 2.1 years ago by prajapatijaimin • 3.1k
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308
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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 2.1 years ago by prajapatijaimin • 3.1k
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326
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The gauge indicates a velocity of $152 m/s$. What is the true speed of the aircraft ?
fluid mechanics updated 2.1 years ago by prajapatijaimin • 3.1k
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1.8k
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Calculate on the stagnation point on the nose of the plane.
fluid mechanics updated 2.1 years ago by prajapatijaimin • 3.1k
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1.5k
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Compute its stagnation properties and the local Mach number.
fluid mechanics updated 2.1 years ago by prajapatijaimin • 3.1k
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The velocity profile within a laminar boundary layer over a flat plate is given by the equation
fluid mechanics updated 2.1 years ago by RakeshBhuse • 3.2k
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