Determine the length of tension anchorage required for the 36 mm diameter plain mild steel reinforcing bars in the canrilever of figuer below. The charactersitic material strengths are feu-30N/mm² and fy-250KN. The ultimate anchorage bond stress. Stress, fou-1.5N/mm² - Anchorage length R25 bars

Determine the length of tension anchorage required for the 36 mm diameter plain mild steel reinforcing bars in the canrilever of figuer below. The charactersitic material strengths are feu-30N/mm² and fy-250KN. The ultimate anchorage bond stress. Stress, fou-1.5N/mm² - Anchorage length R25 bars

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

GIVEN: Solid alumınum bar shown: 4 in. by4 in. E = 10 x 10° psi oy = 36 ksi 4000 2000 1b 4000 16 B 12' REQ’D: A) Load in each section of the bar (state whether C or T) PAB = Pac PCD = B) Maximum axial stress in the bar. In which section does this occur? C) Final length of the bar
idity modulus doengro 17. A 12 mm thick plate is conected to two 8 mm thick plates, on either side through a 16 mm diameter power driven field rivet as shown in the figure below. Assuming permissible shear stress as 90 MPa and permissible bearing stress as 270 MPa in the rivet, the rivet value of the joint is as aeqml 19WOL to da odt ons aasmos m noienet ni mioj по djiw YIVO P/24 F 12mm ↑ P/2 00 8mm 8mm
A plate with width of 300 millimeters and thickness of 20 milimeters is to be connected to two plates of the same width with half the thickness by 25 millimeters by 25 millimeters diameter rivets. The rivets holes have a diameter 2 millimeters larger than the rivetdiameter. The plate is A36 with yield strength F, = 248MP.. Allowable tensile stress on net area is 0.6Fy and allowable bearing stress of 1.3Fy. The rivets are A502, Grade 2, hot-driven rivets with allowable shear stress of 150MPA. 1. Detemine the maximum load that can be applied to the connection with consideration to the yielding failure in the plates. 2. Detemine the maximum load that can be applied to the connection with consideration to the fracture failure in the plates. 3. Detemine the maximum load that can be applied to the connection without exceeding the allowable shearing stress in the rivets. 4. Detemine the maximum load that can be applied to the connection without exceeding the allowable bearing stress between…
The wooden beam shown is made by gluing together planks as shown. 8 kN/m Glue 80 mm A B 80 mm - NA 6 m 80 mm 160 mm Determine the maximum shear stress in the glue in kPa. (2 decimals)
dae 11.25 kips st steel ∙Alum in um A fully bonded aluminum Outer shell and Steel inner core bar is axially loaded. Find the ✓1.25 kips normal stress for the alum', num outer shell. Answer in ksi Given: EA = 11,000 ksi Al Est = 29,000 ks; XAL = 13.5 x 10-6 Y OF Xst = 6.5 x 10-6 1/F dAl = 1.0 in. dst = 0.25 in. AT = 65 °F
The 10-mm-diameter steel bolt in (Figure 1) is surrounded by a bronze sleeve. The outer diameter of this sleeve is 20 mm, and its inner diameter is 10 mm. Est = 200 GPa, Ebr 100 GPa. Figure P P -10 mm -20 mm 1 of 1 Part A If the bolt is subjected to a compressive force of P = 21.9 kN, determine the magnitude of the average normal stress in the steel. Express your answer to three significant figures and include appropriate units. Ost = Submit Part B Obr = Submit 0 Value If the bolt is subjected to a compressive force of P = 21.9 kN, determine the magnitude of the average normal stress in the bronze. Express your answer to three significant figures and include appropriate units. Provide Feedback A Request Answer Value Units Request Answer Units ?
2m 2m 12₂ 2m y 2N/m ✓ 2N/m 2m $ بلا
One bolt 34 in-16 UNF × 2 12 in. SAE grade 5 is subjected to a P load of 6 kip at atension joint. The initial stress is Fi = 25 kip. The stiffness of the bolt and the joint are kb = 6.50and km = 13.8 Mlbf / in, respectively.a) Determine the preload and service load stresses on the bolt. Compare them withthe minimum SAE test strength of the bolt.
The shown plate is 60 mm thick and it is made of Magnesium Am1004-T61. The plate is fitted between the rigid frictionless supports as shown and at T, = 20°C it is stress free. Find the stresses in the x and y directions when the temperature increases to T, = 58°C. %3D 150 mm 150 mm Select one: O x: 0 MPa, y: 42.864 MPa Ox: 22.1 MPa, y: 44.2 MPa Ox: 0 MPa, y: 44.2 MPa Ox: 0 MPa, y: 17.8 MPa O x: 13.2 MPa, y: 44.2 MPa Ox: 0 MPa, y: 67.4 MPa 3:10 PM O G 4) ENG 1/31/2021
The allowable stresses for the splice shown below are the following: 150 MPa. for shear of rivets, 1.35Fy for bearing, 0.6Fy for tension, and Fy = 250 MPa. Note: rivet holes are 2mm bigger than the rivet diameter, middle plate is 20 mm thick. 1. Find the diameter of rivets so that the joint capacity due to shear approximately equals that due to bearing. a. 25 mm b. 28 mm c. 30 mm d. 36 mm 2. Find the maximum safe P without exceeding the allowable shearing stress. a. 884.4 kN b. 938.3 kN c. 878.1 kN d. 848.2 kN 3. Find the maximum safe P without exceeding the allowable tensile stress. a. 579 kN b. 708 kN c. 495 kN d. 692 kN
Consider the singly reinforced beam section given below (left figure). The stress block parameters for the cross-section from IS: 456: 2000 are also given below (right figure). The moment of resistance for the given section by the limit state method is kN-m. 300 mm M25 4-120 Fe415 200 mm 0.42x 0.36 um = 0.48d for Fe415
Directions: Answer the following question to the best of your knowledge. Use clear bond paper for your answer sheet. Use ball pen only. 1. From the given figure below, determine the required cross-sectional area of member BD, DF, and CE if the allowable tensile stress is 65 MPa and allowable compressive stress of 25 MPa. 16 kips 12 kips D 3ft A F E 5000 Ibs 10000 Ibs 4 f t 4 ft 6 ft