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Surface stress induced deflections of cantilever plates with applications to the atomic force microscope: V-shaped plates

J. Appl. Phys. 91, 9354 (2002); doi:10.1063/1.1470240

Issue Date: 1 June 2002

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John Elie Sader
Department of Mathematics and Statistics, University of Melbourne, Victoria, 3010, Australia
Surface stress measurements using atomic force microscopy (AFM) require theoretical knowledge of the surface stress induced deformation of AFM cantilever plates. In a companion paper [J. E. Sader, J. Appl. Phys. 89, 2911 (2001)], a detailed theoretical study of the effects of homogeneous surface stress on rectangular AFM cantilever plates was presented. Since cantilevers of both rectangular and V-shaped geometries are used widely in practice, a corresponding theoretical study for V-shaped cantilevers is presented here. In line with the companion study, an assessment of Stoney's equation is given, together with the presentation of greatly improved analytical formulas and rigorous finite element results. ©2002 American Institute of Physics.
History: Received 15 October 2001; accepted 25 February 2002
Permalink: http://link.aip.org/link/?JAPIAU/91/9354/1
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KEYWORDS and PACS

Keywords
PACS
  • 07.79.Lh
    Instruments, apparatus, and components common to several branches of physics and astronomy Scanning probe microscopes and components Atomic force microscopes
  • 02.70.Dh
    Mathematical methods in physics Computational techniques Finite-element and Galerkin methods
  • 07.10.Pz
    Instruments, apparatus, and components common to several branches of physics and astronomy Mechanical instruments and equipment Instruments for strain, force, and torque
  • YEAR: 2002

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ISSN:
0021-8979 (print)   1089-7550 (online)
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REFERENCES (16)

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  10. G. G. Stoney, Proc. R. Soc. London, Ser. A 82, 172 (1909);
  11. Stoney originally considered the case of uniaxial stress, which was later corrected to account for isotropic and homogeneous surface stresses.
  12. J. E. Sader, J. Appl. Phys. 89, 2911 (2001).
  13. S. Timoshenko and J. N. Goodier, Theory of Elasticity (McGraw-Hill, New York, 1951).
  14. J. N. Reddy, Theory and Analysis of Elastic Plates (Taylor and Francis, Philadelphia, PA, 1999).
  15. Maximum deflections exhibited in practice are typically far smaller than the thickness of the plate.
  16. In the limit as d/b approaches 0.5, the free edges between the two arms of the cantilever collapse to a single point (x = 0; y = 0). This free edge condition does not affect the plate deformation, except for the curvature immediately at this point. Hence, the deformation away from this point is identical to that of a triangular plate with the entire edge (x = 0) rigidly clamped. Behavior at the point (x = 0; y = 0) is not required in surface stress measurements, and is therefore not considered here.
  17. LUSAS is a trademark of, and is available from FEA Ltd. Forge House, 66 High Street, Kingston Upon Thames, Surrey, KT1 1HN, U.K. Quadrilateral elements were used along the skewed rectangular arms of the cantilever, and triangular elements were used near the end tip. Thin plate elements with linear interpolation were used throughout.

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