Interim report Contents 1. Abstract page 2 2. Introduction page 2 3. How the Process Currently Works page 3 4. Two Phase Flow page 4- 6 5. Flow Patterns page 7- 8 6. Interfacial Mass and Energy Exchange page 9 7. Two Phase Flow in Horizontal Pipes page 10 8. Pressure Drop page 11 9. Future Work page 11 10. Timetable page 12 11. References page 13 1
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Volume English 1 teaspoon 1 tablespoon 1 fluid ounce 1 cup 1 pint 1 quart 1 gallon (SI) Metric 1 milliliter 1 liter Symbol tsp. tbsp. (SI) Metric 4.92 milliliters 14.78 milliliters 29.57 milliliters 0.24 liters 0.47 liters 0.95 liters 3.79 liters Symbol ml fl. oz. ml ml c. = 8 fl. oz. pt. = 16 fl. oz. qt. = 32 fl. oz. gal. = 128 fl. oz. Symbol ml = 1‚000 me! I = 1‚000 ml I I I I Symbol English 0.0338140 fluid ounces 33.814022 fluid ounces fl. oz. fl. oz. Multiply the
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lubrication‚ floating ring bearings‚ compressible fluid (gas) lubrication‚ grease lubrication‚ dynamically loaded bearings‚ half speed whirl and stability. Prerequisites: MATH 308‚ MEEN 345 or equivalent. MY OBJECTIVES: To introduce the fundamental physical principles of the classical theory of hydrodynamic lubrication and to review the latest advances and applications to high speed‚ externally pressurized‚ turbulent flow bearings and seals with process fluids. To provide guidance on the important aspects
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ME313L Fluid Mechanic Lab Manual (DRAFT) Pipe Friction Experiment Object: The friction loss in a small-bore horizontal pipe is to be determined over a wide range of Reynolds number. Both laminar and turbulent flow regimes are to be studied. Equipment: Air valve Water manometer Mercury U-tube Isolating tap meter From water supply Needle valve Test tube Figure 1 Pipe friction apparatus A. Laminar Flow The laminar pipe friction apparatus is shown above. It consists of a water loop. The
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speed of a fluid and pressure. The Swiss mathematician and physicist Daniel Bernoulli (1700-1782) discovered the principle that bears his name while conducting experiments concerning an even more fundamental concept: the conservation of energy. This is a law of physics that holds that a system isolated from all outside factors maintains the same total amount of energy‚ though energy transformations from one form to another take place. The principle states that "the pressure of a fluid [liquid
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FMCET Senkottai Village Senkottai Village Madurai – Sivagangai Main Road Madurai – Sivagangai Main Road Madurai - 625 020 Madurai - 625 020 ii ABSTRACT For more than a decade‚ investigations have been conducted to better understand the fluid flow and heat transfer characteristics in silicon-based microchannel heat sinks designed for applications in electronic cooling. These non-circular channels and silicon based microchannel heat sinks combine the attributes of high material compatibility
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saturated vapor enters the turbine. The condenser pressure is 6 kPa. Determine (a) the thermal efficiency. (b) the back work ratio. (c) the net work of the cycle per unit mass of water flowing‚ in kJ/kg. (d) the heat transfer from the working fluid passing through the condenser‚ in kJ per kg of steam flowing. (e) Compare the results of parts (a)–(d) with those of Problem 8.6‚ respectively‚ and comment. 8.8 Plot each of the quantities calculated in Problem 8.6 versus turbine inlet temperature
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industries‚ it is usually involve in large flow network which caused a lot of energy losses during the fluid flow by the fluid friction. Therefore‚ the friction losses along the pipe have to be taken into consideration in order to achieve the better performance for the continuous flow of fluid. The friction factor is essential to the fluid flow and the loss of energy. The loss of energy during the fluid flow is usually due to the dissipation of energy by friction loss along the pipe. If the pipe is of
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the fluid or due to the turbulent behaviour of the flow (Sherwin & Horsley‚ 1996). The continuity equation is a form of the conservation of mass‚ applied to flowing fluids. In the flow the mass flow rate of the fluid entering and leaving the system must be the same (Sherwin & Horsley‚ 1996). It states the product of the density‚ area and velocity of a fluid is a constant in each particular case: ρ1A1v1=ρ2A2v2 Bernoulli’s energy equation is the conservation of energy applied to fluids and
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deflection of jet flow measured from the veritical The negative sign means the Applied Force is opposite to the direction of the inlet jet stream. Nozzle diameter = 8mm Nozzle impact distance = 15mm Bernoulli equation can be used when fluid is considered as an inviscid‚ incompressible and steady flow. |[pic] | (1.4) | With these theory and Bernoulli equation
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