Water B 30° T T 1=2 Mercury- ↑z te N g
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As shown, water flows downward along a pipe inclined at 30° below the horizontal.
The pressure difference between PA and PB is due partly to gravity and partly to friction. The
specific gravity of mercury is 13.55.
(a) Derive an algebraic expression for the pressure difference.
(b) Evaluate the pressure difference (in psi) if L = 5 ft and h = 6 in


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- a)The bore of each cylinder in a six-cylinder car engine is 45 mm and the stroke for each piston is 125 mm. calculate the cubic capacity of the engine in cubic centimetres (cm3 ); and calculate the clearance volume per cylinder for a compression ratio, r, of 8.75. b) The bore of each cylinder in a four-cylinder four-stroke internal combustion engine is 38 mm and the stroke of each piston is 165 mm. During testing, the engine runs at 180 revolutions per minute (rpm) with a pressure-volume indicator diagram showing a mean net area of 3.4 cm2 and a diagram length of 1.2 cm. The pressure scale on the indictor diagram is set to 150 kN/m2 per cm. Calculate the mean effective pressure (m.e.p) and the indicated power developed by this four-cylinder four-stroke engine.Moving to another question will save this response. estion 46 What is the mass of a body in grams if it has a kinetic energy of 94.6N-m when moving at 2.25m/s? →→ Moving to another question will save this response. OLO L2.1 Please help. Written on paper not typed on computer or keyboard please. Need help both questions. Please include all units, steps to the problem and information such as its direction or if it is in compression or tension. Thx.
- *29. ssm The drawing refers to one mole of a monatomic ideal gas and shows a process that has four steps, two isobaric (A to B, C to D) and two isochoric (B to C, D to A). Complete the following table by calculating AU, W, and Q (including the algebraic signs) for each of the four steps. B -800.0-K isotherm -400.0-K isotherm 200.0-K isotherm D Volume PressureIf 16 oz = 1lb followed by 200lb = 1T followed by 1oz =28g followed by 1lb= 0.45kg. Followed by 1T= 0.9 t 670 t to T 670 t =__TConvert 22C to Fahrenheit.
- kindly help me with this problem Use free floating decimals in all your calculations and in expressing your final answers.• Solve problem SYSTEMATICALLY and NEATLY thank you! kindly follow this format GIVEN,REQUIRED,SOLUTIONQuestion 6 a) The bore of each cylinder in a six-cylinder car engine is 45 mm and the stroke for each piston is 125 mm. calculate the cubic capacity of the engine in cubic centimetres (cm³); and calculate the clearance volume per cylinder for a compression ratio, r, of 8.75. b) The bore of each cylinder in a four-cylinder four-stroke internal combustion engine is 38 mm and the stroke of each piston is 165 mm. During testing, the engine runs at 180 revolutions per minute (rpm) with a pressure-volume indicator diagram showing a mean net area of 3.4 cm² and a diagram length of 1.2 cm. The pressure scale on the indictor diagram is set to 150 kN/m² per cm. Calculate the mean effective pressure (m.e.p) and the indicated power developed by this four-cylinder four-stroke engine. c) Figure Q6c shows a pulley system with a suspended load w of 2000 N. Calculate the following: (i) (ii) (iii) (iv) The effort force (FEffort) necessary to lift and hold a load of 2000 N. The ideal mechanical advantage…13. The amount of heat (Hth, thermal energy) stored in rocks, m = 500 kg, S = 840 J/(kg °C), Tfinal =50°C, Tinitial = 40°C is: ·Hth = 19*10E(6) Joules. ·Hth = 4.2 * 10E(6) Joules. %3D ·Hth = 4.2*10E(4)Joules. %3D
- Please help in all subparts Correctly. (Gpt/Ai wrong ans not allowed)MDI stands for _________ ___________ ________.Problem 2 An Air Force Research Lab engineer is asked to evaluate the maximum theoretical work that could be produced by the first stage turbine section of an experimental jet engine. Test stand measurements provide the following information: a. Entering air conditions: 1400 K, 8 bar b. Exiting air conditions: .8 bar Part 1: Since you don't have a mass flow rate measurement, what will be the units will you report maximum theoretical work in? Part 2: Write the first law equation for your control volume showing all terms. What assumptions will you make to simplify the equation. Part 3: Pin down the outlet state on a notional T-s diagram for air (just show the two isobars). Why did you select this point? Part 4: What assumption about the properties of air will you make in order to solve this problem? Part 5: Use the appropriate form of the 'Tds' equation and the air tables to solve for the exit state. Part 6: Calculate the max theoretical work



