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Combustion and Gas turbine

Shortcuts: Differences, Similarities, Jaccard Similarity Coefficient, References.

Difference between Combustion and Gas turbine

Combustion vs. Gas turbine

Combustion, or burning, is a high-temperature exothermic redox chemical reaction between a fuel (the reductant) and an oxidant, usually atmospheric oxygen, that produces oxidized, often gaseous products, in a mixture termed as smoke. A gas turbine, also called a combustion turbine, is a type of continuous combustion, internal combustion engine.

Similarities between Combustion and Gas turbine

Combustion and Gas turbine have 4 things in common (in Unionpedia): Diesel engine, Exhaust gas, Internal combustion engine, Redox.

Diesel engine

The diesel engine (also known as a compression-ignition or CI engine), named after Rudolf Diesel, is an internal combustion engine in which ignition of the fuel which is injected into the combustion chamber is caused by the elevated temperature of the air in the cylinder due to mechanical compression (adiabatic compression).

Combustion and Diesel engine · Diesel engine and Gas turbine · See more »

Exhaust gas

Exhaust gas or flue gas is emitted as a result of the combustion of fuels such as natural gas, gasoline, petrol, biodiesel blends, diesel fuel, fuel oil, or coal.

Combustion and Exhaust gas · Exhaust gas and Gas turbine · See more »

Internal combustion engine

An internal combustion engine (ICE) is a heat engine where the combustion of a fuel occurs with an oxidizer (usually air) in a combustion chamber that is an integral part of the working fluid flow circuit.

Combustion and Internal combustion engine · Gas turbine and Internal combustion engine · See more »

Redox

Redox (short for reduction–oxidation reaction) (pronunciation: or) is a chemical reaction in which the oxidation states of atoms are changed.

Combustion and Redox · Gas turbine and Redox · See more »

The list above answers the following questions

Combustion and Gas turbine Comparison

Combustion has 168 relations, while Gas turbine has 302. As they have in common 4, the Jaccard index is 0.85% = 4 / (168 + 302).

References

This article shows the relationship between Combustion and Gas turbine. To access each article from which the information was extracted, please visit:

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