Open AccessBook
Peterson's Stress Concentration Factors
Walter D. Pilkey
- 01 Jan 1997
1.2K
TL;DR: In this article, the authors present an approach for reducing the number of cycles of alternating and static stress in a two-dimensional problem with respect to a given r D or r H 76.
read more
Abstract: Index to the Stress Concentration Factors. Preface for the Third Edition. Preface for the Second Edition. 1. Definitions and Design Relations. 1.1 Notation. 1.2 Stress Concentration. 1.3 Stress Concentration as a Two-Dimensional Problem. 1.4 Stress Concentration as a Three-Dimensional Problem. 1.5 Plane and Axisymmetric Problems. 1.6 Local and Nonlocal Stress Concentration. 1.7 Multiple Stress Concentration. 1.8 Theories of Strength and Failure. 1.9 Notch Sensitivity. 1.10 Design Relations For Static Stress. 1.11 Design Relations for Alternating Stress. 1.12 Design Relations for Combined Alternating and Static Stresses. 1.13 Limited Number of Cycles of Alternating Stress. 1.14 Stress Concentration Factors and Stress Intensity Factors. References 2. Notches and Grooves. 2.1 Notation. 2.2 Stress Concentration Factors. 2.3 Notches in Tension. 2.4 Depressions in Tension. 2.5 Grooves in Tension. 2.6 Bending of Thin Beams with Notches. 2.7 Bending of Plates with Notches. 2.8 Bending of Solids with Grooves. 2.9 Direct Shear and Torsion. 2.10 Test Specimen Design for Maximum Kt for a Given r D or r H 76. References. Charts. 3. Shoulder Fillets. 3.1 Notation. 3.2 Stress Concentration Factors. 3.3 Tension (Axial Loading). 3.4 Bending. 3.5 Torsion. 3.6 Methods of Reducing Stress Concentration at a Shoulder. References. Charts. 4. Holes. 4.1 Notation. 4.2 Stress Concentration Factors. 4.3 Circular Holes with In-Plane Stresses. 4.4 Elliptical Holes in Tension. 4.5 Various Configurations with In-Plane Stresses. 4.6 Holes in Thick Elements. 4.7 Orthotropic Thin Members. 4.8 Bending. 4.9 Shear and Torsion. 5. Miscellaneous Design Elements. 5.1 Notation. 5.2 Shaft with Keyseat. 5.3 Splined Shaft in Torsion. 5.4 Gear Teeth. 5.5 Press- or Shrink-Fitted Members. 5.6 Bolt and Nut. 5.7 Bolt Head,Turbine-Blade, orCompressor-Blade Fastening (T-Head). 5.8 Lug Joint. 5.8.1 Lugs with h d 0 . 5. 5.8.2 Lugs with h d 0 . 5. 5.9 Curved Bar. 5.10 Helical Spring. 5.10.1 Round or Square Wire Compression or Tension Spring. 5.10.2 Rectangular Wire Compression or Tension Spring. 5.10.3 Helical Torsion Spring. 5.11 Crankshaft. 5.12 Crane Hook. 5.13 U-Shaped Member. 5.14 Angle and Box Sections. 5.15 Cylindrical Pressure Vessel with Torispherical Ends. 5.16 Tubular Joints. References. Charts. 6. Stress Concentration Analysis and Design. 6.1 Computational Methods. 6.2 Finite Element Analysis. 6.3 Design Sensitivity Analysis. 6.4 Design Modification. Index.
read more
Chat with Paper
AI Agents for this Paper
Find similar papers on Google Scholar, PubMed and Arxiv
Write a critical review of this paper
Analyze citations of this paper to find unaddressed research gaps
Citations
Effect of Constraint on Creep Behavior of 9Cr-1Mo Steel
TL;DR: In this paper, the effect of constraint on the creep rupture behavior of 9Cr-1Mo steel was investigated and the authors found that the curvature of the U-notch in a plain cylindrical creep specimen of 5 mm diameter increased with the increase in degree of constraint and applied stress.
43
Mechanical behaviour of epoxy/silica nanocomposites: Experiments and modelling
TL;DR: In this paper, a study on the effect of the curing cycle on the mechanical properties of nanocomposites is carried out, considering two different curing conditions, and it is shown that while nanomodification always enhances the fracture toughness of the epoxy resin, the strength and the notch strength are shown either to increase or to decrease, depending on the curing process of specimens.
43
Fatigue strength reduction factors at rivet holes for aircraft fuselage lap joints
TL;DR: In this article, a series of fatigue tests on aluminium alloy sheet coupons with an open hole and filled hole subjected to remote tension, pin loading and out-of-plane bending have been carried out.
41
Post-fire compressive behaviour of carbon fibers woven-ply Polyphenylene Sulfide laminates for aeronautical applications
TL;DR: In this paper, the influence of fire exposure on the residual compressive behaviors of carbon fibers woven-ply Polyphenylene Sulfide has been investigated for aeronautical applications, showing that prior fire exposure is highly detrimental to the compressive mechanical properties as the residual strength and stiffness decrease by approximately 75% and 55% respectively.
41
Quantitative fractography and modelling of fatigue crack propagation in high strength AerMet®100 steel repaired with a laser cladding process
TL;DR: In this paper, the authors report a study of the fatigue endurance of AerMet®100 steel components repaired by the laser cladding process, and a fracture mechanics based model to predict the fatigue fatigue of repaired components.
41
References
A numerical solution for axially symmetrical and plane elasticity problems
D.S. Griffin,R.B. Kellogg +1 more
TL;DR: In this paper, a finite difference method is presented for the solution of axially symmetrical and plane elasticity problems which makes efficient use of the high-speed digital computer and is ideally suited to the treatment of both simply and multiply connected regions with irregular boundary shapes, temperature distributions, body force distributions, and any physically admissible combination of boundary tractions and displacements.
27
A survey of post-peterson stress concentration factor data
S.J. Hardy,N.H. Malik +1 more
TL;DR: In this paper, a collation of such published data is presented for studies conducted since 1974, for various combinations of geometry, discontinuities and loadings, and a useful aid in the design analysis of engineering components is presented.
26
Related Papers (5)
R. E. Peterson,R. Plunkett +1 more
- 01 Jan 1974
Raymond Jefferson Roark,Warren C Young +1 more
- 01 Jan 1938
Jaap Schijve
- 01 Jan 2001