An energy audit for a hotel (Anantara Iko mauritius resort and villa) including introductions, abstract, literature review, improvement, referencing .Around 10000 -15000
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An energy audit for a hotel (Anantara Iko mauritius resort and villa) including introductions, abstract, literature review, improvement, referencing .
Around 10000 -15000
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- Please explainHello I have two pictures with some questions Id like to get answers to! Short and great explanations please thank you !Oil shale is a type of solid fuelAn example of non-flow process is a piston assembyWork is the thermal energy transferredPeat is a type of liquid fuelA.) If all 4 statements are trueB.) If 3 of the 4 statements are trueC.) If 2 of the 4 statements are trueD.) If only 1 of the 4 statements is trueE.) If none of the 4 statements is true
- I hope you can help me thank youWhich of the following formulas describe the thermal efficiency of a cycle? Select all that applies. 1 - qin/qout worknet/qout worknet/qin 1 - qout/qinSolve using the Mollier Diagram. Plot the data and how you got the data (process how you used the diagram) to determine the items below. Please only use this Mollier diagram below and show process by drawing on it. Thank you Steam enters a turbine at 3.0 MPaa and 700 deg. C and expands isentropically to 0.098325 MPavac. Steam = 4.5 undergoing an irreversible adiabatic process under the same properties, determine: (a) the actual work done (KJ) if AKE = 0 and h2' = 2,400 KJ/kg; Ans: (b) Determine the following: actual quality at exhaust. Ans: c) Ideal turbine work. Ans: d) Ideal steam temp at the exhaust. Ans._ e) Degree Superheat of the steam at turbine inlet. Ans_ (I only have this one question left. thank you)
- Solve using the Mollier Diagram. Plot the data and how you got the data (process how you used the diagram) to determine the items below. Please only use this Mollier diagram below and show process by drawing on it. Thank you Steam enters a turbine at 3.0 MPaa and 700 deg. C and expands isentropically to 0.098325 MPavac. Steam = 4.5 undergoing an irreversible adiabatic process under the same properties, determine: f) actual entropy at steam outlet. Ans g) Actual temp. of steam at the exhaust. Ans. h) irreversible adiabatic expansion efficiency. Ans. i) AS for irreversible adiabatic process_ (Please solve all subparts, this is my last question. Thank you)Show Complete SolutionASSIGNMENT ABO0UT THERMODYNAMICS
- The left side of this equation tells how much energy Q the cylinder gives to the water while it cools. The right side of this equation tells how much energy Q the water and aluminum cup absorb from the cylinder to warm up. Because it is the same energy, they are equal. What is known in this equation? Mcyl 411.7 g, malum 46.5 g, malum+water = 175 g Can you find: mwater =? g Twater = Talum = 20°C (water and cup of room temperature) 90°C, T; = 35°C (hot cylinder and cool "cylinder+cup+water" temperatures) Tcyl kCal Calum = 0.22, Cwater 1 (specific heat of water and aluminum, measured in units kg-°C What are we looking for is Ccul - How we find it? Plug all the numbers into the equation (1), Ccul will be one unknown which you can calculate from the equation. Important, convert all the masses from grams to kilograms! After you find Ccyl, compare it to known value for the copper 0.093(our cylinder is made out of copper). |Ceyl -0.093| % : · 100% 0.093Answer question 3, 4, 5 showing fully all the steps. Solution should be simplified and easy to understand as much as possible!PRAUO ACTIVITY NO.6 IN THERMODYNAMICS PROCESSES OF IDEAL GASSES (PROBLEM SET) Directions: 1. Solve the problems that are assigned to you. 2. One problem for each student. 3. Present the solution properly to each problem (copy the problem first, given, required, solution, formula, derivation of formula, then put a box on the final answer). Express your answer in three decimal places. 4. Please check the deadline of submission and be on time. Answer the following questions. 1. A scuba tank contains 1.5 kg of air. The air in the tank is initially at 15 °C. The tank is left near an engine exhaust line, and the tank's pressure doubles. The constant volume specific heat is 0.7186 kJ/kg- K. Determine: a) the final temperature. b) the change in internal energy.