Answered: TURBINE its definition its principle…

Engineering

Mechanical Engineering

TURBINE its definition its principle its diagram and names of part

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Related questions

Q: The efficiency at the best operating point is:

A: The best operating point is that point at which a pump is least prone or least probable to failure…

Q: Why are Francis and Kaplan turbines generally consideredunsuitable for hydropower sites where the…

A: Francis and Kaplan turbines could work on a wide range of heads and flow rates. But there are so…

Q: ID/S. Part b.) Determine the entropy production (o) of this turbine.

Q: Write any four advantages of Vertical Axis wind turbine.

A: Vertical axis wind turbine - it is a type of turbine which has the blades mounted on the top…

Q: Identify the most common water turbines and the limitations that exist within these different types?

A: A water turbine is a device which is used to produce the energy .these turbines are installed in…

Q: Pelton turbine is the only type that is mostly used these days. It is also called free jet turbine…

Q: (d) If petroleum is a non-renewable resource, briefly explain how it can be prevented from…

A: to explain the following (d) If petroleum is a non-renewable resource, briefly explain how it can be…

Q: Identify the main types of Hydro power turbines and the difference between them.

A: Solution: There are two main types of hydro turbines: impulse and reaction. 1) IMPULSE TURBINE In…

Q: fluid mechanics what are the limitations of the different types if water turbines?

Q: Bas engines WiLh plication ?.-

Q: Explain the wind turbine its part and function of each parts, how it will convert energy?

A: I have mentioned the part names and pics with the help of Power point (for the better understanding…

Q: Turbines are to be installed where the net head is 400 ft andthe fl ow rate 250,000 gal/min. Discuss…

A: Given data: The net head, H = 400 ft. The flow rate, Q = 250,000 gal/min. Select two turbines of…

Q: derivation of steady flow energy equation from first principles

Q: Work out put =0.6 Parameters Inlet Temperature Pressure Velocity Outlet X = 0.85 50 kPa 50 m/s 350…

Q: The following particulars refer to a row velacity-Compounded impulse wheel which foams of a the…

A: Thermodynamics : It is a branch of science which deals with work, heat, energy. Also, it studies…

Q: 1150 A Parson's reaction turbine has the following data for a particular stage; turbine speed is…

A: Solution:

Q: Thermo-Fluid I

A: Stagnation PointA stagnation point, in fluid dynamics, is a point in the flow field where the local…

Q: Define the Maximum Power Generation by a Wind Turbine.

A: Step-1 Wind turbine- The device used to transform the kinetic energy of wind into mechanical energy…

Q: he date for a certain installation are as follows Net Head = 454 m, BP = 57,200 bkw, n = 750 rpm,…

A: Given:H=454 mP=57200 KWN=750 rpm

Q: A compressor draws in 500 cfm of air whose density is 0.079 lb/ft and discharges it with a density…

Q: 68. Water at a rate of 1 m'/s enters a small hydraulic turbine from the horizontal supply line,…

Q: ow that the index 'n' of polytropic expansion in a turbine of infinitesim stage efficiency np is…

Q: [ In a simple turebine setup; a compressor drawn in air from the atmosphere at 3ook and Compressor…

A: Here we will take the compression and expansion to be isentropic as there is no mention of…

Q: The range of discharge pressure of the blower is 500mmH2O ~ 2.0kgf/cm2, guage. How to convert this…

A: Given Data: Pressure range, P= 500 mm H2O~ 2.0 kgf/cm2

Q: 100 R, Po1 =200 psia, an :11

A: As a piece of a task on microjet motor plan and production, this paper depicts exhaustively every…

Q: can a wind turbine have an efficiency of 85% ? Give reasons to support your answer

A: No, a wind turbine can not have an efficiency of 85%. Wind turbine efficiency is the amount of…

Q: For the following adiabatic Turbine, calculate: 1- adiabatic efficiency (+)- 2- the mass flow rate…

A: P1= 2 MPaT1= 350∘CP2= 100 kPaT2= 150∘CW˙out= 2.5 MW= 2.5(1000) kW

Q: Total to static efficiency of an axial turbine is 0.85 and Stagnation enthalpy at inlet: 4300 kJ/kg…

A: Write the formula for the total to static efficiency of the axial turbine. ηts=Wth01-h3 Here, ηts is…

Q: Approximate the theoretical power in wind moving at a speed of 6 m/s with an air temperature of 40°F…

Q: There are two broad categories of turbomachinery, pumps and turbines. Discuss the differences…

A: PUMPS :- It is turbo machinery which will convert mechanical energy into fluid(pressure head) energy…

Q: 5. The velocity of steam at section in a scaling nozzle can reach to the critical point. 6. The…

A: Solution: Given Data: To Find: Fill in the blanks.

Q: Select one limitation of the use of the Bernoulli Equation? А. Must consider frictional effects for…

A: GIVEN- TOPIC -FLUID MECHANICS DETERMINE CORRECT OPTION OF LIMITATIONS OF USE OF…

Concept explainers

Applied Fluid Mechanics

A fluid is a substance that is continuously deformed by the application of shear stress. The rate of deformation of a fluid depends on its viscosity. The fluid tries to flow when it interacts with some other system.

Question

Question:-

TURBINE its definition its principle its diagram and names of parts

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

SEE SOLUTION Check out a sample Q&A here

Step 1

VIEW

Step 2

VIEW

Step by step

Solved in 2 steps with 1 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.

Similar questions

2nd Quiz: (Answer only one question of the following two questions) Q1) Find: (a) inlet temperature (T1 =?), (b) mass flow rate of R-134a (m =?), (c) exit diameter (D2 =?), (d) the rate of heat transferred to the surroundings (Qout =? ). P2 = 1MPA T2 = 70°C m Y2 = 70 = Compressor W in = 100 (W) R-134a P = 500KP. Qout (sat. vapor)(1) m. Y1 = 20 () D = 0.5 (cm)
1. Gas is compressed in a reciprocating compressor from 33 kPa to 89 kPa. The FAD is 14 dm3/s. The clearance ratio is 0.09. The expansion part of the cycle follows the law pV 1.2 = C. Calculate the swept volume and the volumetric efficiency.
Answer correctly please. I will rate accordingly.
Solve it correctly please. I
Question ONE A- For Fig.1, state the type of each turbine and state what is the range of Head of the water with which it operates. (c) (a) (b) 스폰 Fig.1 (d)
مراد جبار فرحان In a gas turbine engine (A, = 2.85 A2, p1 = 1.14 p2, p1 = 100.5 kPa, T, = 11 °C, v1 = 107 m-s1, V2 = 785 m-s", A, = 2.4 m?), calculate the thrust force. %3D %3D ===
Please show complete solution. Thank you!
I need the answer as soon as possible
i need the answer quickly
Question B3 The engine of an aeroplane is equipped with an ideal convergent nozzle with an area ratio Ainlet 2.035 ( -A-2.035), as in Figure Q-B3. The aeroplane is flying at an altitude of 11 Aexit km where the atmospheric pressure and temperature are 0.23 bar and 216K respectively. You may assume the combustion gases entering the nozzle have the same property as air (i.e. y=1.40, R=287 J/kgK and Cp-1004.5J/kgK). Page 6 Question B3 continued inlet exit Amles/Aexit -AVAJ-2.035 Figure Q-B3 a) If the nozzle operates at its critical condition, calculate: the inlet Mach number M;. nozzle's exit velocity V, the inlet stagnation pressure Por- the inlet static pressure FG The stagnation Aj P, and the nozzle's gross thrust per unit exit area temperature of the gases entering the nozzle is To 1200 K. b) If the stagnation pressure at the inlet of the nozzle is reduced to 80% of its value in part (a), determine the exit static temperature 7;, the nozzle's gross thrust per unit exit area FG. The…
Superheated steam at 40 bar absolute and 500°C flows at a rate of 250 kg/min to an adiabaticturbine, where it expands to 5 bar. The turbine develops 1500 kW. From the turbine thesteam flows to a heater, where it is reheated isobarically to its initial temperature. Neglectkinetic energy changes.(a) Write an energy balance on the turbine and use it to determine the outlet streamtemperature.(b) Write an energy balance on the heater and use it to determine the required input (kW) tothe steam.(c) Verify that an overall energy balance on the two-unit process is satisfied.(d) Suppose the turbine inlet and outlet pipes both have diameters of 0.5 meter. Show that itis reasonable to neglect the change in kinetic energy for this unit.
no hurry ............. a very good handwriting with every step to be mentioned to understand the answer easily step to follow given requirement solution result if not followed the above steps , ready for consequences i want the solution with a very good handwriting