outlet and the flow Velocity to be constent. FindB. An inward flow reaction turbine Ŝ supplying weter at arete G00 litre/seconde with a relocity of flow 6m/s.The relocitylf mls restecfilely. Assuming the discharge to the Fedi radiat atl MIN LTE1/1at the Periphery and the wheel Welocity at intet are 24mls cand4:20 AMO 17% CIne loane engple at inlet.he head of water over the Lekeed.

Given; Discharge rate = 600 liters/s Velocity of flow = 6 m/s The velocity at periphery , u1=24 m/s…

(he head of water over the Lelkeed. B. An inward flow reation turbine & Supplyiny water at outlet and the flow Velocity to be constent. Find lfmls restectiuely. Assuming the discharge to the entr radialt at rate 600 litre /secande with arelocity of flow Gm/ls. The relocity .The bane angle at inlet. he head of water over the Lekeed.

(he head of water over the Lelkeed. B. An inward flow reation turbine & Supplyiny water at outlet and the flow Velocity to be constent. Find lfmls restectiuely. Assuming the discharge to the entr radialt at rate 600 litre /secande with arelocity of flow Gm/ls. The relocity .The bane angle at inlet. he head of water over the Lekeed.

Refrigeration and Air Conditioning Technology (MindTap Course List)

8th Edition

ISBN:9781305578296

Author:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson

Publisher:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson

Chapter40: Typical Operating Conditions

Section: Chapter Questions

Problem 10RQ: The seasonal energy efficiency ratio (SEER) includes the energy used in the _____and _____cycles.

See similar textbooks

Similar questions

i need some one explian the TS digram Rankine Cycle
Fast pls solve this question correctly in 5 min pls I will give u like for sure Mnty If you are running 3500lbs PSI of steam thru the turbine and your governor trips at 4200 PSI. What is your percentage of increase pressure required to reach the High Limits?
2- Diesel engine, six cylinders is tested at 4750 rpm, the pressure and temperature of the air entering the engine are 1.2bar, and 25 if the bore of cylinder is 80 mm and stroke 120 mm ,take air fuel ratio is 12:1, the specific fuel consumption is 0.52kg/kWh, and the brake power is equal 94 kW find the following: fuel consumption m'f = kg/ sec the air consumption engine capacity.: the flow rate of air intake to cylinder the Volumetric efficiency
For two row velocity compounded simple impulse turbine wheel derive the expressions for Diagram Power and Diagram Efficiency and also prove that : i. (P )max = 8 Cb? ii. ( na )max = Cos'ai
Drive Velocity Triangle For Axial Mixed Flow For Francis Turbine.
A Kaplan turbine of 100 B.H.P. is working under a headof 5 in and running at 210 R.P.M.The discharge through the tur.bine is 1*80 m°/sec.If now the turbine is allowed to work under a head of 15 m,what would be its new speed, discharge and power ?
The impeller of a centrifugal pump having external and internal diameter 500mm and 250mm respectively, width at out let 50mm and running at 200rpm works against a head of 48m. The velocity of flow through the impeller is constant and equal to 3m/s the vanes are set back at an angle of 400 at outlet. Determine A.inlet vane angle B.workdone by the impeller on water per second c.manometric efficiency
Q14: Arancis turbine operates under a head of (24.5m) and consumes (10.5m³/s) of water whilst runnlag at (225 r.p.m). The velocity of flow at inlet (6.5 m/s), the inlet blade angle is (65), assume hydraulic efficiency is (90%) and no volume and mechanical losses and velocity of whirl at exit equal to zero. Calculate i) Diameter of the runner at entry, ii) Specific speed of turbine runner. Q=TD.B.VP)
Considering the wind speed of 5 m/s, air density of 1 kg/m3, exponentfactor is 0.20 and turbine diameter of 100 m:a. Calculate the turbine electrical power considering the maximumBitz limit,b. The original wind speed was taken at a height of 10 m,calculate the turbine power if it is now installed at 50 m height.c. In what condition a capacity factor of 73% can be reached bythis turbine.
A petrol engine is having, stroke length of 200 mm and clerance length (clerance gap) of 20 mm. Then the compression ratio of such engine will be a. 12 b. 11 c. 0.01 d. 10
A simple jet carburetor is required to supply 5 kg of ai and 0.5 kg of fuel per minute. The fuel specific gravity is 0.75. Thrnea'r is initially at 1 bar and 300 K. Calculate the throat diameter or ir choke for a flc ty ocity of 100 m/s. Velocite oefficient is 0.8. If the pressure drop acit 1 1he fuel metering orific orifice diameter assuming. Caf .60 and= 1.4. 80 of that of the choke. calculate
PROBLEM 4 A centrifugal pump delivers 26 Vs against a total head of 16m at 1460 rpm. The impeller diameter is 0.5 m A geometrically similar pump of 30 cm diameters running at 2900 rom. Assuming equal efficiencies between the two pumps. Calculate the head, and A. 11.52 m B12.03 m C.40.7 m D. 6.09 m discharge required. A. 8.01/s 865/s c1 23 Vs D. 7.5 l/s