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Steam and Gas Turbines Practice Test: Turbine Blade Profile
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Avg score: 56% • Most missed: “In vortex fluid flow velocity is ______________ to the distance from the axis li…”
Turbine Blade Profile topics include: Turbine, impulse and reaction blade profiles, blade entrance and exit angles, losses and geometry of impulse blade profiles and passages, gauging and pitch and free and forced vertex. Steam turbine blades are critical components in power plants. They convert the linear motion of high temperature and high pressure steam into a rotary motion of the turbine shaft.  Here are some things to know about turbine blade profiles: The leading edge is where the gas flow enters the profile while the trailing edge is where the gas leaves the profile. The specific... Show more
Steam and Gas Turbines Practice Test: Turbine Blade Profile
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25 Questions

1. Angle between surface of target and plane perpendicular to the nozzle central line is called as _______
2. In forced vortex all fluid particles rotate with the ________________
3. Blade exit angle is a measure for _________
4. Steam is directed towards rotor by _________
5. A ___________ drawn from the head of turbine blade to tail is called as chord.
6. Stagnation enthalpy is _______ in turbo machine along the radial direction.
7. In forced vortex the total head _______ with radius.
8. If specific volume of steam increases its blade height _______
9. Stagnation enthalpy is _________ at intake and discharge.
10. Blade entrance angle is represented by _________
11. Angle between chord and turbine rotation is called as _________
12. Flow through turbo machinery is ________
13. Radial equilibrium theory is more important for Radial flow machines.
14. Vorticity is _______ in the core region.
15. Maximum chamber is represented by ____________
16. Angle made by the relative velocity vector entering the fixed blades to the horizontal line is called as ____________
17. Different pressures are maintained on ________ sides of reaction turbine blades.
18. In parsons turbine to increase area between blades its height is to be ________
19. Blade exit angle is represented by _______
20. Losses that occur when steam is supplied from boiler to turbine is called as ___________
21. Losses occurred while passing through blades are called as ________
22. Ratio of actual velocity to velocity of case lossless flow is called as _______
23. Difference between actual enthalpy of working fluid to case enthalpy of isoentropic flow is called as _______
24. In reaction turbine direction of fluid flow is changed drastically.
25. Nozzle angle is represented by ______

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