Determine the value of the uniformly distributed loadd "w".What is the numeric value of C1 ( 1st constant)?Dtermine the deflection at midspan. Question textA rectangular beam is supported at both ends. It carries two concentrated load of170KN, a clockwise moment of 130kN-m, and a uniformly distributed load "w". Themodulus of elasticity of the beam is 190GP.. Solve the following if the reaction atpoint B is 178.66666666667KN, upward.BEAM DIMENSION: Width = 180mm , Height = 310mmNOTE: b = 3m; Also, DON'T FORGET TO TYPE DOWN THE CORRECT UNITS(IF NEEDED)wMImImimDetermine the value of the uniformly distributed load "w". Answer for part 1kN/mWhat is the numeric value of C1 (Ist Constant)? Answer for part 2kN-m2Determine the deflection at midspan.Answer and unit for part 31

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Answered: Determine the value of the uniformly…

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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A:Y 211O 2_531929016114... -> A rod is composed of an aluminum section rigidly attached between steel and bronze sections, as shown in Figure below. Axial loads are applied at the positions indicated. If P = 11 KN and the cross sectional area of each rod is 312.5 mm, determine the stress in each section. 4P Steel Bronze |Aluminum 609.6 mm 914.4 mm 762 mm
A rectangular beam is supported at both ends. It carries two concentrated load of 10kN, a clockwise moment of 180kN-m, and a uniformly distributed load "w". The modulus of elasticity of the beam is 140GPa. Solve the following if the reaction at point B is 305.2kN, upward. BEAM DIMENSION: Width = 140mm , Height = 360mm NOTE: b = 4.5m What is the numeric value of C1 (1st Constant)? Determine the deflection at midspan.
A beam ABC with an overhang from B toC supports a uniform load of 200 lb/ft throughout itslength (see figure). The beam is a channel section withdimensions as shown in the figure. The moment of inertiaabout the z axis (the neutral axis) equals 8.13 in4.(a) Calculate the maximum tensile stress σt andmaximum compressive stress σc due to theuniform load.(b) Find the required span length a that results inthe ratio of larger to smaller compressive stressbeing equal to the ratio of larger to smaller tensilestress for the beam. Assume that the totallength L =a + b = 18 ft remains unchanged.
P A B 1m E 1m 2m The simply supported beam shown has a solid rectangular cross section having beam width of 130mm and a height of 200mm. Assuming values of P = 25KN, w = 30 kN/m, and E = 5m, determine: 1) The max tensile bending stress in MPa (enter this value into D2L answer box, in MPa). Exactly where does this occur along the beam? (4 sigs) 2) The max shear stress in MPa. Exactly where does this occur along the beam? ( 4 sigs) Your Answer:
.
An aluminum bar having a cross-sectional area of 160 mm2 carries the axial loads as shown in the Figure below. Assume that the bar is suitably braced to prevent buckling and E = 70000 MPa. The length of each bars are follow: B, = 0.8 m; B, = 1.0 m; B3= 0.6 m. Determine the axial stress of bar B; in MPa. 35KN B1 B2 ВЗ ... 10KN 15KN 30KN A 218.75 B 125 C 62.5 D 31.25
3. Two bars are made of a material with the stress-strain diagram as shown. Find the cross-sectional area of each bar so the bars fail at the same time with the load is P = 4 kips. Use a factor of safety of 1.8. 3 ft 4 ft P B σ (ksi) 25 20- 15 10- 5H 0 0 tension. compression 0.20 0.40 0.60 0.80 e (in./in.)
The cantilever beam shown is an aluminum pipe that has an outside diameter of 114 mm and an inside diameter of 97.3 mm. A moment of 3 kN-m is applied at the free end. Find the rotation at the free end of the pipe. Neglect the weight of the pipe. М 33KN.m 2m Mod. of Mod. of Coeff, of Elasticity Rigidity G Thermal Ultimate Strength Density kg /m3 x 10 Tensile Yield Strength F, MPa Expansion a m/m/C x 10-6 Poisson's MPa MPa MPa Ratio Material x 10 x 10 Tens. Comp. Shear Steel ASTM A36 or A501 7.85 207 83 250 400 11.7 0.25 Steel (high-strength low-alloy) ASTM A992 7.85 207 83 345 450 11.7 0.25 Steel AISI 1020 hot-rolled 7.85 207 79.3 210 380 11.7 0.25 Steel AISI 1040 hot-rolled 7.85 207 79.3 290 520 11.7 0.25 Stainless steel 7.85 200 80 280 580 410 11.7 0.25 (annealed) Cast iron (gray) 7.21 103 41 140 550 220 10.6 0.26 Aluminum allov 2.64 70 28 240 260 190 23.6 0.33 6061-T6 Magnesium alloy 1.794 45 17 210 280 140 26.1 0.34 Titanium alloy 4.40 114 45 900 970 690 9.7 Nominal Outside Inside…
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A steel cantilever beam 6 m in length is subjected to a concentrated load of 120 N acting at the free end of the bar. The cross section of the beam is shown below. deep. Determine the magnitude and location of the maximum tensile and compressive bending stresses in the beam. As usual, neglect the weight of the beam. 4mm 120 N 1mm 1mm 6mm 6m 1mm 4mm
The beam has a rectangular cross section and is subjected to the loading shown. Determine the components of stress ox, oy, and Txy at point B. 800 N B 1000 N 15 mm 20 mm 20 mm 15 mm 100 mm 10 mm
PROBLEMS 237. The lower ends of the three bars in the figure are at the same level before the rigid homogeneous 18Mg block is attached. Each steel bar has an area of 600mm² and E=200GPa. For the bronze bar, the area is 900mm² and E-83GPa. Find the stress developed in each bar. BRONZE 1.6M STEEL 1M 18Mg STEEL 1M ТЕСНА

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Determine the value of the uniformly distributed loadd "w". What is the numeric value of C1 ( 1st constant)? Dtermine the deflection at midspan.