Anderson's theory of faulting
Anderson's theory of faulting is a seminal framework in structural geology that explains the initiation, orientation, and mechanics of faults in the brittle upper crust as a function of the regional stress field. Developed by Scottish geologist Ernest Masson Anderson, the theory posits that fault planes form at optimal angles to the principal stress directions to accommodate shear failure under varying tectonic conditions.[1] The theory rests on two key assumptions applicable to shallow crustal levels: the Earth's surface represents a free boundary with no shear stress, implying that the principal stresses align with the vertical and horizontal directions; and the vertical stress arises primarily from the lithostatic load of the overlying rock column.[2] These assumptions lead to three fundamental tectonic regimes defined by the relative magnitudes of the principal stresses (denoted σ₁ as the maximum compressive, σ₂ intermediate, and σ₃ minimum): the gravity regime where σ₁ is vertical, favoring extensional normal faulting; the thrust regime where σ₃ is vertical, promoting compressional reverse faulting; and the wrench regime where σ₂ is vertical, resulting in strike-slip faulting.[1] Building on the Coulomb-Mohr failure criterion, Anderson's model predicts conjugate fault pairs inclined at approximately 30°–45° to the maximum compressive stress direction, yielding characteristic dips of about 60° for normal faults, 30° for low-angle reverse (thrust) faults, and near-vertical planes for strike-slip faults, assuming a typical rock friction angle of 30°.[2] First outlined in Anderson's 1905 address to the Edinburgh Geological Society and elaborated in his 1942 monograph The Dynamics of Faulting and Dyke Formation with Applications to Britain, the theory has profoundly influenced modern tectonics, seismology, and rock mechanics by providing a basis for inferring paleostress orientations from fault geometries observed in the field.[1][3]Introduction
Historical development
Ernest Masson Anderson, a Scottish geologist trained at the University of Edinburgh, first proposed his theory of faulting in 1905 during a presentation to the Edinburgh Geological Society. In his paper "The dynamics of faulting," Anderson introduced a classification of faults based on the orientation of the three principal stresses, assuming that one principal stress acts vertically due to the influence of the Earth's free surface. This work marked a pioneering application of stress analysis to geological structures, predating widespread recognition of strike-slip faulting, as evidenced by the 1906 San Francisco earthquake.[4] Anderson's ideas drew on late 19th-century foundations in rock mechanics. His development occurred in the context of early 20th-century advances, including his appointment to the Geological Survey of Great Britain in 1903, which provided field opportunities in Scotland to observe fault patterns, and growing interest in tectonic processes following continental drift hypotheses.[4] These influences allowed Anderson to integrate continuum mechanics with empirical observations, establishing a theoretical basis for fault initiation under varying stress regimes. Anderson expanded and formalized his framework in the book The Dynamics of Faulting and Dyke Formation with Applications to Britain, first published in 1942 and revised in a second edition in 1951. This seminal text elaborated on the mechanics of faulting, incorporating the Coulomb failure criterion and applications to British geology, solidifying the theory's role in structural geology.[5] The centennial of Anderson's 1905 paper was marked by reflections on its lasting influence, particularly in a 2008 review that analyzed global seismicity data to affirm the prevalence of Andersonian fault types in earthquake focal mechanisms. This recognition underscored the theory's foundational status, with over a century of refinements in rock mechanics and tectonics continuing to build upon its core assumptions.[6]Core principles
Anderson's theory of faulting establishes that shear failure in the brittle crust occurs on planes inclined at approximately 30° to 45° relative to the maximum principal compressive stress direction (σ₁), positioning the fault roughly perpendicular to the minimum principal stress (σ₃). This orientation minimizes the shear stress required for failure while maximizing resistance due to normal stress on the plane, assuming frictional sliding as the dominant mechanism. The specific angle depends on the internal friction angle of the rock, typically around 30° for common crustal materials with a friction coefficient of about 0.6.[7][8] Central to the theory is the assumption that the Earth's free surface imposes a boundary condition where no shear stress acts on horizontal planes, making the vertical direction one of the principal stress axes. Consequently, the vertical stress (σᵥ) aligns with either σ₁, σ₂, or σ₃, simplifying the analysis of fault orientations in a three-dimensional stress field. This vertical principal stress arises from the overburden pressure and gravitational loading, influencing how horizontal tectonic forces interact with the crust.[7][8] The theory classifies faults into three primary types based on which principal stress is vertical, directly linking stress regimes to fault geometry:- Normal faults, formed when σ₁ is vertical (overburden dominates) and σ₃ is horizontal, accommodating crustal extension with typical dips of around 60°.
- Reverse and thrust faults, occurring when σ₃ is vertical and σ₁ is horizontal, reflecting horizontal contraction with shallower dips of about 30°.
- Strike-slip faults, developing when σ₂ is vertical and both σ₁ and σ₃ are horizontal, producing near-vertical fault planes for lateral shear.[7][8]