Determine in flow stream, Mechanical Engineering

Assignment Help:

Derive and solve a model of an insulated water tank with a changing level (i.e., changing tank volume).

There is only one in ow stream with a flow rate of 1 kg/sec for t < 0 and 0.9 kg/sec for t  0.

The out flow rate depends upon the level, H, within the tank and is given by mout = kv √H where kv = 0:8kg=(m0:5s). The tank is tted with an electric heater that inputs Q = 100kW (constant), and the cross-sectional area of the tank is 1:1m2. Derive both the mass and energy balances, determine the steady state conditions at t < 0, and determine via numerical simulation the impact of the changing in flow rate at t ≥ 0.


Related Discussions:- Determine in flow stream

Applied Elasticity, Can you prove an equation from Plane Stress and Plane s...

Can you prove an equation from Plane Stress and Plane strain?

Determine the maximum shear stress, Determine the maximum shear stress: ...

Determine the maximum shear stress: A beam of triangular cross section of base width 120 mm & height 80 mm is subjected to a shear stress force of 3 kN. Determine the maximum

What is enthalpy, Enthalpy defines as heat content of a chemical system.

Enthalpy defines as heat content of a chemical system.

Airport drainage, Airport Drainage: Rainwater should be quickly taken...

Airport Drainage: Rainwater should be quickly taken away from the runway, taxiway and apron areas. For drainage of runway and taxiway, a cross-slope of 1.5 per cent on either

Causeways, Paved Dips: Paved dips, also known as bed level causeways,...

Paved Dips: Paved dips, also known as bed level causeways, are structures consisting of gentle and shallow depressions in the road where the water is allowed to flow over the

High pressure die casting process, what is the working princile of high pre...

what is the working princile of high preesure die casting process

Chemical machining., chemical milling is used in aircraft plant to create p...

chemical milling is used in aircraft plant to create pockets in wing sections made of an aluminium alloy. the starting thickness of one work part is 20 mm.a series of rectangular s

Strengh of material, case study of thermal stresses and composite bar

case study of thermal stresses and composite bar

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd