Textbook Solutions: Fluid Mechanics, Heat & Mass Transfer, Aerodynamics
This page is being continuously updated with complex (text-book type) problems in Fluid Mechanics, Heat Transfer, Aerodynamics, Mass Transfer, Combustion and Thermodynamics. The solutions to compressible flows including sub-sonic, sonic and supersonic flows inside a converging-diverging nozzle will be presented.
This is a very useful case which has frequent engineering applications.
Even though the complicated definite integration is possible analytically, this is the time the introduce a simple method based on properties of sections. Note that the numerator of expression for centre of pressure is the "Second Moment of Inertia" or simply the Moment of Inertia about a "chosen axis" - typically the free surface of the liquid. The denominator is the "Moment of Area" about the same axis as chosen above - also known as "Statical Moment". Thus:
For the circular plate:
Note about location of centre of pressure in the coordinate direction perpendicular to the depth of liquid column:
A metallic block is floating along with a wooden block as shown in the figure below. If this metallic block falls into the tank, calculate the new depth of floatation and height of water level in the tank.
The method of relating two phenomena with some come feature is a powerful tool to both understand and remember the concepts. Following table summarizes key parameters which are analogous in the field of fluid flow (momentum transfer), heat transfer and mass transfer.
The designs of heat exchangers are the most predominant application of conductive heat transfer with such boundary conditions. The temperature profile in walls of a water-cooled internal combustion engine is also subject to this combination of boundary conditions though heat generation is not present in this application. Some applications can be current carrying conductor cooled by convection on both inner and outer diameters, nuclear fission in a annular cross-section cooled by convection on both the inner and outer radii.
The governing equation and general solution of the differential equation is given by
Heat flow is assumed positive from left to right. Hence, the convective heat transfer on left face is negative if ambient temperature is < wall temperature on the left face!
Note velocities in pipe branches 1-2, 2-3 and 3-4 are not known in advance and hence the loss coefficients KMN cannot be adjusted to same velocity. Note that the junction losses at node 2 can be incorporated either in K12 or in K23 and K24. It is more convenient to club the node loss in K12 as appropriate assignment into K23 and K24 will involve extra calculations.
This is a non-linear equation in V23 and needs to be solved using trial-and-error or iterative approaches. Microsoft Excel Goal Seek utility can be used to solve this equation as well. A good initial guess would be required.
A more compact approach in terms of fluid resistances can be used as demonstrated below.
Thus, we have 3 equations and 3 unknowns – but they are still non-linear and needs to be solved using iterative method.
A reducing bend having diameters D upstream and d downstream, has water flowing through it at the rate of m [kg/s] under a pressure of p1 bar. Neglecting any loss is head for friction calculate, the horizontal and vertical components of force exerted by the water on the bend.
This is the force acting on the fluid and only means to apply the force on the fluid is the walls of the pipe. Hence, from Newton’s third law, and equation and opposite force will act on the pipe.ΔΓX = m * [u2X - u1X] = FΓX. Thus: FΓX = m * [u2 cos(θ) - u1]
For gases at very high pressure and those in liquid state such as Liquified Petrolium Gas (LPG), the accuracy of ideal gas equation falls sharply. Many improvizations have been made and SRK equation is one such method. The approach is demonstrated using following sample problem:
A gas cylinder with a volume of 5.0 m3 contains 44 kg of carbon dioxide at T = 273 K. estimate the gas pressure in [atm] using the SRK equation of state. Critical properties of CO2 and Pitzer acentric factor are: Tc = 304.2 K, pc = 72.9 atm, and ω = 0.225.
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