| 301. |
In a gas turbine power plant, a regenerator increases the
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Answer:
Option (c) |
| 302. |
The thermal efficiency of a gas turbine cycle with ideal regenerative heat exchange is
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Answer:
Option (c) |
| 303. |
With the increase in pressure ratio thermal efficiency of a simple gas turbine power plant with fixed turbine inlet temperature
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Answer:
Option (c) |
| 304. |
The combines cycle power plants are more appropriate for
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Answer:
Option (c) |
| 305. |
The combined cycle power plants are more appropriate for capacity factors of
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Answer:
Option (b) |
| 306. |
In a two stages gas turbine plant reheating after first stage
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Answer:
Option (b) |
| 307. |
In a two stage gas turbine power plant intercooling and reheating
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Answer:
Option (a) |
| 308. |
A jet aircraft is powered by
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Answer:
Option (c) |
| 309. |
For a jet propulsion unit, ideally the work of compressor and that of gas turbine are
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Answer:
Option (b) |
| 310. |
In a closed cycle operation of gas turbines
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Answer:
Option (d) |