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Steam enters a rotor of an axial turbine with an absolute velocity V1 320 m/s at...
Steam enters a rotor of an axial turbine with an absolute velocity V1 = 710 m/s at an angle α1 = 67.5°. The rotor speed is U = 200 m/s. The rotor blades are equiangular so that β2= -β1 and W2=0.91 W1. (a) Draw the velocity triangles and show the velocity components along the radial and tangential directions. Find the following. (b) the relative flow angle β1. (c) the magnitude of the velocity V2of the steam that leaves the rotor,...
> Click Submit to complete this assessment Question 8 Question 8 24 points Save Answ Steam enters a rotor of an axial turbine with an absolute velocity V1 - 350 m/s at an angle = 70". The axial velocity remains constant (Va1-Va2) and W1=W2. The blade speed is U-165 m/s. The rolor blades are equiangular. Draw the velocity Thanges. Find (a) the rotor blades angle degree (b) the specific work done = kJ/kg (c) the blade efficiency % Click Submit...
The axial flow steam turbine rotor shown in Fig. P12.69 has a blade outer radius RO 2.40 ft, a blade inner radius Ri 2.00 ft, a steam inlet pressure p1 200 psia, a steam inlet density p1- 0.296 lbm/t3, and an inlet absolute velocity V1 1000 f/s making an angle of 70° with the axial direction. The steam outlet pressure p2 50 psia and outlet density is 0.1014 Ibm/t3. B2 40 The rotor rotates at 3600 rpm. Using a blade...
P 8.1 (100 points) The stator exit flow angle in an axial steam turbine is 69o. The flow angle of the relative velocity leaving the rotor is 65°. Steam leaves the stator at V2- 190 m/s, and the axial velocity is Vx2 0.46U. At the exit of the rotor blades the axial steam velocity is V-0.45U. The mass flow rate is m2-2.2 kg/s. Draw the velocity triangles and find (a) the flow angle of the relative velocity entering the rotor;...
Q2 Figure 2.1 shows the velocity diagram for an axial turbine stage. The turbine rotor blade speed is 80 m's. Exhaust gas flow through the turbine stage with a constant axial velocity (2) at 90 m/s. List of relative and absolute flow angles at the rotor inlet and outlet are given in APPENDIX D for each student, respectively. At rotor inlet At rotor outlet B3 Cx2 = 90 m/s B2 Cx3 = 90 m/s W2 0.3 Cys 44 U =...
The rotor shown below rotates with an angular velocity of 2000 rpm. Assume that the fluid enters in the radial direction and the relative velocity is tangent to the blades across the entire rotor. Find the exit normal velocity (ft/s) and exit velocity of the blade in terms of inlet. Draw the inlet and outlet velocity triangles. Is the device a pump or a turbine? Explain. Hint: create a velocity triangle at (1) and (2) and compare them. Does the...
The steam at a velocity of 600 m/s is directed to the blades of an impulse turbine at an angle of 25o to their motion. The blade velocity is 225 m/s and the exit angle of the blades is 30o. If the blade velocity coefficient (k) is 0.9,Calculate: a)The inlet angle of the blade. b)The power developed per kg of steam supplied per second.
TQi The rotor and stator rows arrangement of an axial compressor stage and their general velocity diagrams are shown in Figure 1.1 (a) and (b), respectively. The compressor rotor blade speed is set at 100 m's and the inlet absolute flow velocity for rotor (C1) and stator (C:) are given in APPENDIX A (Each student will have different data) Consider normal stage condition and constant axial flow throughout the stage at 50 m's 01 C 0 SS 93 ROTOR t=100...
please solve 5(b) and 6 (a and b) fluid machinery
b)An inward flow reaction turbine works under a head of 100m. The inlet and outlet diameters of the runner are 1.2 m and 0.6 m, respectively. The width of the runner is 150 mm, which is constant throughout. The velocity of flow at the outlet is 6 m/s. The blade angle at the outlet is 15. The hydraulic efficiency is 0.9. Calculate the following: ) The speed of the Turbine...
The following data is given for a Francis turbine with an axial discharge Overall efficiency Hydraulic efficiency Power produced Net head 75 % 78 % 148.25 kW 7.62 m 3.179 m/s The wheel peripheral velocity at inlet The radial velocity of the flow at inlet The runner diameter at inlet 11.738 m/s 0.4047 m The guide blade angle (with respect to the radial direction) is 57.4 36 5 30.8 28.8 e following data is given for a Fra... The following...