A flanged cross section is Used to suppaut the lcadsshown on the beamon the extpage. The dimen glons oFthe ghape are given. Congider the entire om lengthg Hhe beam and defermine.a:) he maximum tengion bending stres atalong he beam and,anylocationB) te maximum compreggion ben ding stress at anyJocatien along the beam.20aml00 mm4.5 YNJOmmIs kN Im310 mm270malAI1. 5m1.2m1o mm20nm

Determine the cross-sectional area and moment of inertia. The cross-sectional area of the beam is A.…

A flanged cros5 section is Used to suppaut the lcads shown on the beam on the et page. The dimen glonsoF he ghape are given. Congider the entire om length g the beam and delermin! a) the maximum tengion oending stres at amy location along the beam and, maximum compreggion ben ding gtress at any Jocation along the beam. b) te 20 am lo0 mm 4.5 YN JOmm- Is EN Im 310 nm 270 pa Al 1. 5m 1.2m 10 mm 20nm

A flanged cros5 section is Used to suppaut the lcads shown on the beam on the et page. The dimen glonsoF he ghape are given. Congider the entire om length g the beam and delermin! a) the maximum tengion oending stres at amy location along the beam and, maximum compreggion ben ding gtress at any Jocation along the beam. b) te 20 am lo0 mm 4.5 YN JOmm- Is EN Im 310 nm 270 pa Al 1. 5m 1.2m 10 mm 20nm

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

y = EI 1 B For the beam and loading shown, determine Part 1 out of 3 (a) the equation of the elastic curve for portion AB of the beam, WO 2 L x Wo -L/2- 1 120 10 X X 1
In the assembly shown. the block has a weight w = 200 lbs and the cord is attached to the pin at B. The pulleys have radi of rt = 2 Tn. and r2 1 În. Neglect the mass of the pulleys and the link. Pulley Pulley A 45 12 Compute the reaction at the ĩnk AB In lbs." 250 260 280 B.
he 40-Kip vertical load at Joint C i the stec ying table. The cross-sectional ay er is given in the table. The elastic t (in.) of Joint C is most ‘nearl; FE CIvIL PRACTICE EXAM iven in the el truss shown below produces the foroles e rea of each member is 4.0 in’, and the length S modulus of steel is 29,000 ksi. The downward y: Member Rorce ki Length, L (kips) i AB 500 BC 492 cp 750 AD -30.0 BD 2250
J- A distributed load op w (kulm) is applied over the entire tength OF a simply supported beam Gm long . The beam section is as shown. Determine the maximum value OF w iF Of Ś 1OMP , and yE 800KP. 80 mm X 200 mm 360mm 200mm
(2) 4 0 5 211 5 4 #9 4 "1 16 #3" ft-k fé = 3 ksi, M = 90 NWC. The section is cracked. Computer the bending stresses in the beam by using transformed-area metho
At which point on the design P-M interaction diagram is the design flexural strength largest? O Pure compression Pure tension Balanced failure point (CCL limit) O TCL limit Beam condition (Pn = 0) %3D //img00.zhaopin.cm
Q-1 Link-2, shown in the figure, is 30 mm wide, has 12 mm diameter bearings atthe ends, and is cut from low carbon steel bar having a minimum yield strength of190 MPa. The end-condition constants for link-2 are C = 1 and C = 1.2 for bucklingin and out of the drawing, respectively.a) Draw necessary and clear free-body diagrams to determine the reactions atthe supports and the load on both member-2 and member-3. b) Determine a suitable thickness for link-2, based on a design factor of safetyηD = 4, and considering a material having E = 207 GPa, and a minimum yieldstrength Sy = 350 MPa.c) Determine the stress and resulting factor of safety for each pin, and state yoursuggestions in case of design factors less than 4.
Determine the force in member DI of the loaded truss. Enter a positive number if in tension, negative if in compression. 4L B 5 m Answer: DI = i Save for Later 6L 6L D E 6L -5 m E H |Η 5 m AB=BC=CD= DE = EF = FG 4L L F L G Attempts: 0 of 1 used Submit Answer
Determine the design key points A, B, C, D and E on the section capacity line (N-M, interaction diagram) for the column section shown in Figure below for the case where 4N24 bars in each face. Bending takes place about the x-axis, f'= 40 MPa, fy-500 MPa, and E,=200 GPa 4N24 4N24 a D O O O y 600 mm O 72 mm x - - 72 mm I 600 mm 71
Question 22 Form the given beam loaded has shown, Ely = MAT + RĄ2² – P(x – )2 +C1 - Ely = 글MA22 + 금RAz' - 공P(z-)3 + Ciz+ Ca 3 + C1a + C2 Let P=58 kN, L = 19 m P в с D -L/3- L/2 -L/2- Determine the bending moment at point A.
*4-76 The C83400-red-brass rod AB and 2014-T6-alu- minum rod BC are joined at the collar B and fixed connected at their ends. If there is no load in the members when T₁ = 50°F, determine the average normal stress in each member when T₂ = 120°F. Also, how far will the collar be displaced? The cross-sectional area of each member is 1.75 in². 3 ft B 2 ft C