Elastic constants quantify the relationship between stress and elastic strain through the constitutive matrix. Young's modulus E describes uniaxial stiffness; shear modulus G describes resistance to shear; bulk modulus K describes resistance to volume change. These constants depend on atomic bonding strength and crystal structure, and they determine stiffness, damping, and elastic energy storage.
Begin with uniaxial stress-strain relationships to understand Young's modulus, then extend to shear and volumetric deformations. Use ultrasonic measurements, impulse excitation, and dynamic mechanical analysis to measure elastic constants experimentally.
Elastic constants do not scale linearly with bonding strength. Shear modulus depends more on bonding directionality than on bond strength alone. Also, elastic constants vary significantly with temperature and sometimes show anomalous behavior near phase transitions.
You have already seen from the stress-strain curve that in the elastic region, stress and strain are linearly proportional, and the slope is a material property. The central insight of elasticity theory is that this linear relationship generalizes: for any combination of applied stresses in three dimensions, the resulting strains are linear combinations of all the stress components, and the coefficients form a matrix of elastic constants. For isotropic materials (properties the same in all directions), only two independent constants are needed to fully describe all possible elastic deformations — typically Young's modulus E and Poisson's ratio ν.
Young's modulus E is the slope of the uniaxial stress-strain curve in the elastic region: E = σ/ε. It tells you how stiff a material is — how much it resists elongation under tension. Steel has E ≈ 200 GPa; aluminum ≈ 70 GPa; rubber ≈ 0.01–0.1 GPa. Critically, E is set by atomic bonding: it reflects the curvature of the interatomic potential energy well near the equilibrium spacing. Atoms held together by deep, steep potential wells (strong, stiff bonds) resist displacement more and give higher E. This explains why you cannot significantly change stiffness through heat treatment or alloying — those processes modify microstructure and strength, but barely affect the fundamental bond stiffness. If a design requires higher stiffness, you must select a different material class.
Poisson's ratio ν captures lateral contraction under axial extension: ν = −ε_transverse/ε_axial. Most structural metals have ν ≈ 0.25–0.35. An incompressible material (rubber-like) approaches ν = 0.5; a cork has ν ≈ 0, which is why corks can be pushed into bottles without bulging sideways. Shear modulus G = E/(2(1+ν)) describes resistance to shear — the angular distortion of an element under shear stress. Bulk modulus K = E/(3(1−2ν)) describes resistance to hydrostatic compression. These four constants are not independent: for an isotropic material, knowing any two determines the other two. This interrelationship means that a material optimized for high stiffness (high E) at low density — a key design driver for aerospace structures — inevitably has a fixed ratio of G and K, constraining the full mechanical response.
Understanding elastic constants as processing-independent material fingerprints is crucial for engineering design. Stiffness requirements (deflection limits, vibration frequencies, buckling loads) constrain your material choices at the very beginning of design — no amount of processing will raise the stiffness of a given material class. Within a class, processing controls strength and toughness. The sequence in materials selection is: stiffness constraint narrows material families; then strength, toughness, corrosion resistance, and cost narrow the specific choice. Elastic constants are the first filter.