Engineering Thermodynamics Exam Review

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Flashcards reviewing key vocabulary and concepts from engineering thermodynamics lecture notes.

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20 Terms

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Specific heat capacity

The amount of heat required to raise the temperature of 1kg of a material by 1°C.

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Thermal diffusivity

The rate at which a material reacts to a sudden change in temperature to regain thermal equilibrium.

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Thermal conductivity

The rate at which heat is transported within a solid material.

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Natural Convection h-value

Typically ranges between 1-10 W/m²K.

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Critical insulation radius

The total wall thickness at which the radial thermal resistance is minimized.

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Lumped mass analysis

Simplifies thermal analysis by neglecting spatial temperature variations within an object.

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Reynolds Number Effect

The heat transfer between a wall and a fluid increases with an increasing Reynolds number.

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Prandtl Number

Indicates how the momentum and thermal boundary layers relate to each other.

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Grashoff Number in Natural Convection

The Grashoff number determines the type of flow in natural convection.

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Colored thermal radiation

Radiation with an intensity that is wavelength dependent.

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Wien's Displacement Law

Heated charcoal reaches its highest temperature when it visually appears white.

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Thermally black body

Has an emissivity of 1.

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Heat Exchanger Outlet Temperature

The outlet temperature of the cold fluid can only be higher than the inlet temperature of the hot fluid in the case of a counter-current heat exchanger or a condensing gas/evaporating liquid.

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Heat Exchanger Capacity Rate

In heat exchangers, the fluid with the smallest capacity rate (mc) experiences the largest temperature change.

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U-value of a Heat Exchanger

Depends on the geometry and the type of fluid.

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Syngas

A mixture of CO and H₂.

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Complete Combustion Process

Occurs when C, H, and S are fully converted into CO₂, H₂O, and SO₂.

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Lean Combustion Process

A process where λ> 1.

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Adiabatic Combustion Process

In an adiabatic process with combustion in an open thermodynamic system where work is done, Σw=Σp Np[h+(h-h°)]P-ΣR NR [h+(h-h°)]R.

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Adiabatic Flame Temperature

The temperature of the gases after complete combustion, without heat or technical work exchanged with the environment.