3- A bracket is riveted to a column by 6 rivets of equal size as shown in Fig.3 It carries a load of 60 kN at a distance
Posted: Tue Jun 07, 2022 1:23 pm
FACTORS A. [ 4-23 CHARTS OF THEORETICAL STREMAXNCENTRATION 29 1.10. 14 124 010 0.15 0 20 030 1/6 nCURE A-255 Rectangular filleted bar in trmaien or simple - F/A, where 4 and is the thickness 1 14 12 IP 2.5 80 FIGURE A-23-13 -beved 8²/14. 08 402 13 102 0.10 Q.15 rjd Grooved round D14-15 L.13 PNS 0.20 FM har in temion-Fi Hot rolled Quenched and drawn steels (Bhn > 2001 Annealed steels (Bhn 200) Aluminum alloys 02 2 Notch radius r. mm GURE 7-11 Notch-sensitivity curves for materials in reversed oon. For larger notch radii use the values of corresponding to .-4 mm. Pulised Ground. 49 Machired or cold drawn ork as Us 04 As forges 0.3 02 0.1 0.4 0.8 1.0 1.2 Tensile strength S... GP 1.4 10 FIGURE 7-8 Surface-finish modification factors for steel. These are the , factors for use in Eq. (7-15). Nichumvity 0.95 K₁ D 0.1 02 03 0.4 0.5 05 0.7 DA d/u FIGURE A-23-12 Plate loaded in tension hy a pin through a hole dold. where 4-(-). When clearance est, in- crease K, 35 to 50 percent. [37. St. Fricht and H. N. Hill, Stress Conciation Faciers around Central Curular Hele in a Plate Loaded through Pin in Hole, J. Appl. Mechanis, l. 7. n. 1, p. A-S, March, 10 1.4 GP S 1.0 on 06- 04 02 Stewis Alum alloy 1.0 3.0 2.0 FIGURE 7-11 Notch-sensitivity charis for steels and 2024-T wrought Notch radius F, mm aluminum alloys subjected to reversed bending or reversed axial loads. For larger nnich radii use the values of --- w. 4.0 Dermation for Pr. Reliability R Standardized variable & Reliability factor i 0.50 0 0.50 1.000 1.288 0.597 1.645 0.568 2.326 0814 3.050 0.753 3.719 0.702 4.265 0.6.39 4.753 0620 5.199 0.554 5.612 0.331 5.997 0.520 0.90 0.9009 0.99999 69895 050409 0.539 0.50 900 90 3.0 2/2 K₁ 2.6 22 18 04 14 TR ## PALES No-959 walo Djd- 102 -1.05) 1.0 0.05 0.30 0.10 0.15 0.25 0.20 r/d FIGURE A-23-6 Rectangular filleted bar iu bending. Mijl, where ead/2₁/1³/12, and is the thicknen.