Compressors, Gas Turbines and Jet Engines
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- Subject
- Compressors, Gas Turbines and Jet Enginesmechanical-engineering-mcqs › compressors-gas-turbines-and-jet-engines
- Published
- 24 Jan 2019
- Last updated
- 28 May 2026
Explanation
Option A is incorrect because large gas turbines typically use axial flow turbines rather than radial inflow types. Option B is incorrect since gas turbine blades differ in design compared to steam turbine blades. Option C is correct: gas turbine blades exhibit impulse characteristics at the hub and reaction characteristics at the tip. Option D is incorrect as gas turbines generally use air cooling, not both air and liquid cooling. Therefore, option C is the accurate statement.
More Compressors, Gas Turbines and Jet Engines MCQs
Practice related questions from the same subject.
- 1.Identify the incorrect statement from the following options:
- 2.Which of the following statements about gas turbines is accurate?
- 3.Identify the incorrect statement from the following:
- 4.Which of the following statements about gas turbines is accurate?
- 5.Identify the incorrect statement from the following options:
- 6.Which of the following statements is accurate?
- 7.Identify the incorrect statement regarding gas turbines:
- 8.After combustion gases pass through the turbine in a jet engine, where are they expelled?
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