Catalog / Mechanical Engineering Cheatsheet
Mechanical Engineering Cheatsheet
A quick reference guide covering fundamental concepts, formulas, and principles in mechanical engineering. Ideal for students, engineers, and professionals.
Thermodynamics
Basic Concepts
Zeroth Law: |
If two thermodynamic systems are each in thermal equilibrium with a third, then they are in thermal equilibrium with each other. |
First Law: |
Energy can neither be created nor destroyed. Conservation of energy: ΔU = Q - W, where U is internal energy, Q is heat added, and W is work done. |
Second Law: |
The total entropy of an isolated system can only increase over time or remain constant in ideal cases. Entropy is a measure of disorder. |
Third Law: |
As temperature approaches absolute zero, the entropy of a system approaches a minimum or zero value. |
Enthalpy (H): |
A thermodynamic property defined as H = U + PV, where U is internal energy, P is pressure, and V is volume. |
Entropy (S): |
A measure of the disorder of a system. ΔS = Q/T for a reversible process at constant temperature. |
Thermodynamic Processes
Isothermal: |
Constant temperature process. PV = constant. |
Adiabatic: |
No heat transfer. PVγ = constant, where γ is the heat capacity ratio (Cp/Cv). |
Isobaric: |
Constant pressure process. V/T = constant. |
Isochoric (Isometric): |
Constant volume process. P/T = constant. |
Polytropic: |
Process described by PVn = constant, where n is the polytropic index. |
Throttling: |
Adiabatic process where enthalpy remains constant. Used in refrigeration. |
Heat Engines and Refrigerators
Heat Engine Efficiency (η): |
η = W/QH = 1 - (QC/QH), where W is work done, QH is heat input, and QC is heat rejected. |
Carnot Efficiency (ηCarnot): |
ηCarnot = 1 - (TC/TH), where TC is the cold reservoir temperature, and TH is the hot reservoir temperature (in Kelvin). |
Coefficient of Performance (COP) - Refrigerator: |
COPR = QC/W = QC/(QH - QC) |
Coefficient of Performance (COP) - Heat Pump: |
COPHP = QH/W = QH/(QH - QC) |
Fluid Mechanics
Fluid Properties
Density (ρ): |
Mass per unit volume: ρ = m/V |
Specific Weight (γ): |
Weight per unit volume: γ = ρg, where g is acceleration due to gravity. |
Specific Gravity (SG): |
Ratio of a fluid’s density to the density of water: SG = ρfluid/ρwater |
Viscosity (μ): |
Measure of a fluid’s resistance to flow. Dynamic viscosity. |
Kinematic Viscosity (ν): |
Ratio of dynamic viscosity to density: ν = μ/ρ |
Surface Tension (σ): |
Force per unit length acting at the interface between two fluids. |
Fluid Statics
Pressure (P): |
Force per unit area: P = F/A |
Hydrostatic Pressure: |
P = ρgh, where h is the depth from the surface. |
Buoyancy (FB): |
Upward force exerted by a fluid that opposes the weight of an immersed object: FB = ρfluidVdisplacedg |
Manometry: |
Use of liquid columns to measure pressure differences. |
Fluid Dynamics
Continuity Equation: |
A1V1 = A2V2 (for incompressible fluids) |
Bernoulli’s Equation: |
P + (1/2)ρV2 + ρgh = constant (along a streamline) |
Reynolds Number (Re): |
Re = (ρVD)/μ, where V is flow velocity, D is characteristic length, and μ is dynamic viscosity. Indicates laminar (Re < 2100) or turbulent flow (Re > 4000). |
Darcy-Weisbach Equation: |
ΔP = f (L/D) (ρV2/2), where f is the friction factor. |
Materials Science
Material Properties
Young’s Modulus (E): |
Measure of stiffness or resistance to elastic deformation: E = Stress/Strain |
Poisson’s Ratio (ν): |
Ratio of transverse strain to axial strain. |
Yield Strength (σy): |
Stress at which a material begins to deform plastically. |
Tensile Strength (σu): |
Maximum stress a material can withstand before breaking. |
Hardness: |
Resistance to localized plastic deformation (e.g., indentation). |
Ductility: |
Ability of a material to deform plastically before fracture. |
Stress and Strain
Stress (σ): |
Force per unit area: σ = F/A |
Strain (ε): |
Deformation per unit length: ε = ΔL/L |
Shear Stress (τ): |
Stress acting parallel to a surface. |
Shear Strain (γ): |
Angular deformation. |
Hooke’s Law: |
σ = Eε (in the elastic region) |
Material Types
Metals: High strength, ductility, and thermal/electrical conductivity. Examples: Steel, Aluminum, Copper. |
Ceramics: High hardness, brittleness, and resistance to high temperatures. Examples: Alumina, Silicon Carbide. |
Polymers: Low density, flexibility, and can be easily molded. Examples: Polyethylene, Polypropylene. |
Composites: Combination of two or more materials to achieve enhanced properties. Examples: Carbon fiber reinforced polymer (CFRP). |
Mechanics of Materials
Stress Analysis
Axial Stress (σ): |
Stress due to axial force: σ = P/A, where P is the axial force and A is the cross-sectional area. |
Bending Stress (σb): |
Stress due to bending moment: σb = My/I, where M is the bending moment, y is the distance from the neutral axis, and I is the moment of inertia. |
Shear Stress in Beams (τ): |
τ = VQ/Ib, where V is the shear force, Q is the first moment of area, I is the moment of inertia, and b is the width of the beam. |
Torsional Shear Stress (τ): |
τ = Tr/J, where T is the torque, r is the radius, and J is the polar moment of inertia. |
Principal Stresses: |
Maximum and minimum normal stresses at a point. |
Beam Deflection
Deflection Formulas: |
Vary based on loading and support conditions. Common cases include cantilever beams and simply supported beams with various loads. |
Cantilever Beam with Point Load at End: |
Maximum deflection (δ) = (PL3)/(3EI), where P is the load, L is the length, E is Young’s modulus, and I is the moment of inertia. |
Simply Supported Beam with Uniform Load: |
Maximum deflection (δ) = (5wL4)/(384EI), where w is the uniform load per unit length. |
Failure Theories
Maximum Shear Stress Theory (Tresca): Failure occurs when maximum shear stress exceeds the shear strength of the material. |
Distortion Energy Theory (von Mises): Failure occurs when the distortion energy reaches the distortion energy at yield in a simple tension test. |
Maximum Principal Stress Theory: Failure occurs when the maximum principal stress exceeds the tensile strength of the material. |