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Fluid Mechanics

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2
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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 3.7 years ago by snadith342 • 20
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Write a short note on Moodys Diagram
fluid mechanics updated 4.1 years ago by saniiphone2378 • 20
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Write short note on aerofoil theory
fluid mechanics updated 4.1 years ago by yerasylmakulbe671 • 10
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Classify lubricating oil using viscosity (SAE) and load severity (API) rating.
fluid mechanics updated 4.1 years ago by krithikkm200 • 10
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The velocity components in two dimensional flow field are as follows 10
fluid mechanics updated 4.1 years ago by abhibrajwasi225 • 20
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Write short note on Minor losses in pipe.
fluid mechanics updated 4.1 years ago by 19bcs3866 • 10
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Explain a Sonic Velocity for Isothermal Process and Adiabatic Process.
fluid mechanics updated 4.1 years ago by thambisrilalith126 • 20
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What is Shock waves? explain about Normal Shock Wave.
fluid mechanics updated 4.1 years ago by thambisrilalith126 • 20
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(Duplicate) take mass density of air $1.205 kg/m^3$ , CD =1.33.
fluid mechanics updated 4.1 years ago by phenjoisilab • 0
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Hydraulic jump Numerical
fluid mechanics updated 4.1 years ago by rjran106 • 20
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Determine the viscosity of the oil.
fluid mechanics updated 4.1 years ago by yerasylmakulbe671 • 10
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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 4.1 years ago by thambisrilalith126 • 20
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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 4.1 years ago by thambisrilalith126 • 20
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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 4.1 years ago by thambisrilalith126 • 20
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For the velocity profile for laminar boundary flow
fluid mechanics updated 4.1 years ago by rjran106 • 20
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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 4.1 years ago by rjran106 • 20
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Compressible Fluid Flow
fluid mechanics updated 4.1 years ago by rjran106 • 20
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Boundary Layer Flows
fluid mechanics updated 4.1 years ago by rjran106 • 20
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Explain the Laval nozzle (convergent-divergent nozzle).
fluid mechanics updated 4.1 years ago by thambisrilalith126 • 20
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Determine the reservoir pressure, temperature and the throat area. Take $\gamma=1.4$.
fluid mechanics updated 4.1 years ago by thambisrilalith126 • 20
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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 4.1 years ago by thambisrilalith126 • 20
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The gauge indicates a velocity of $152 m/s$. What is the true speed of the aircraft ?
fluid mechanics updated 4.1 years ago by thambisrilalith126 • 20
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Calculate on the stagnation point on the nose of the plane.
fluid mechanics updated 4.1 years ago by thambisrilalith126 • 20
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Compute its stagnation properties and the local Mach number.
fluid mechanics updated 4.1 years ago by thambisrilalith126 • 20
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The velocity profile within a laminar boundary layer over a flat plate is given by the equation
fluid mechanics updated 4.1 years ago by rjran106 • 20
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