A gold-alloy microbeam attached to a silicon wafer behaves like a cantilever beam subjected to a uniform load (see figure). The beam has length L = 27.5 µm and rectangular cross section of width b = 4.0 µm and thickness. The total load on the beam is 17.2 %3D %3D µN. If the deflection at the end of the beam is 2.46 µm, what is the modulus of elasticity Eg of the gold alloy? (Use the formulas of Example 9-2.) PROB. 9.3-6 qL? + qLx 2 M = (9-27) qx? + qLx 2 EN" (9-28) %3D 2 qx (3L2 6EI 3Lx + x2) (9-29) qx2 (6L2 - 4Lx + x²) 24EI V = -- (9-30) qL3 -v(L) : (9-31) %3D 6EI -KL) : 8EI (9-32) %3D %3D

A gold-alloy microbeam attached to a silicon wafer behaves like a cantilever beam subjected to a uniform load (see figure). The beam has length L = 27.5 µm and rectangular cross section of width b = 4.0 µm and thickness. The total load on the beam is 17.2 %3D %3D µN. If the deflection at the end of the beam is 2.46 µm, what is the modulus of elasticity Eg of the gold alloy? (Use the formulas of Example 9-2.) PROB. 9.3-6 qL? + qLx 2 M = (9-27) qx? + qLx 2 EN" (9-28) %3D 2 qx (3L2 6EI 3Lx + x2) (9-29) qx2 (6L2 - 4Lx + x²) 24EI V = -- (9-30) qL3 -v(L) : (9-31) %3D 6EI -KL) : 8EI (9-32) %3D %3D

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

20KN 2m 2m Example: (3B): Find the value of the force P to reduce the deflection of point c to the half ? 20(KNA) C B' P
Determine the maximum deflection of a simply supported beam carrying a hydraulic cylinder in a machine used to press bushings into a casting as shown in the figure. The force exerted during the pressing operation in 45 kN. The beam is rectangular, 35 mm thick and 150 mm high, and made of steel (E = 207 Gpa).
H.W A steel bar 160cm long under applied loading as shown in figure 4.Find the elongation of bar,take E=2.1x10 N/cm?. 2 3 solution 9N 3cm 4N 3.Scm 3cm, 11N 6N 50 cm 70cm aocm Activate Windows
H= 55mm A= 40mm R1 R2 B= 55mm C= 50mm R1=13mm H P=2000 N R2= 15mm A B Figure QI: A rectangular plate with holes
The beam is subjected to a point load and a distribution load as shown in Figure 2-1 below.(a) Draw a Shear Force Diagram in the beam ABC interval.(b) Draw a Moment Diagram in the beam ABC interval.(c) If the cross-sectional area is shown in Figure 2-2, how many mm is the neural axis NA from the bottom?(d) Find the second moment of area, INA from the natural axis.(e) Find the maximum shear stress JJ on the stem side at the connection between flange and stem in the beam ABC interval. (f) Find the maximum shear stress mmax in the beam ABC interval.(g) Find the maximum tensile flexural stress mmax, T and maximum compressive flexural stress mmax, C in the beam ABC interval, respectively.
can you help me answer this question using the figure provided? thank you.
A cantilever beam is subjected to an inclined force (P) as shown in Figure 1, the equilibrium normal force component on the cross- sectional area at the point A is (in kN) Figure 1: P 400 kN 30 1000 mm A Area 30 mm 20 mm
A long, slender structural aluminum [E = 69 GPa] flanged shape is used as a L = 9.2-m-long column. The column is supported in the x direction at base A and pinned at ends A and C against translation in the y and z directions. Lateral support is provided to the column so that deflection in the x-z plane is restrained at mid-height B; however, the column is free to deflect in the x-y plane at B. Assume that b; = 102 mm, d = 122 mm, t; = 8 mm, and tw = 6 mm. Determine the maximum compressive load P the column can support if a factor of safety of 2.9 is required. In your analysis, consider the possibility that buckling could occur about either the strong axis (i.e., the z axis) or the weak axis (i.e., the y axis) of the aluminum column. P bf C d Lateral В bracing 2 Determine the moment of inertia with respect to the y and the z axes through the centroid of the cross section area. Answers: ly = i mm“, Iz = i mm4.
Using finite element 1.8 Find the stress distribution in the beam shown in Figure 1.19 using two beam elements. www E, I constant 34 Figure 1.19. LA
2. In a laboratory test of a beam loaded by end couples, the fibers at layer AB in Figure below are found to increase 60 x 10-3 mm whereas those at CD decrease 100 x 103 mm in the 200-mm-gage length. Using E=70 GPa, determine the flexural stress in the top and bottom fibers. 200 mm 30 mm B 120 mm 30 mm Hello sir, please solve detailed details, boring, new article, I didn't understand anything, please sir, thank you sir. A how detailed solution
A fiber reinfored rod contains 50 volume percent glass fiber ( E = 700 GPa) and 50 volume percent plastic ( E = 7 GPa) . The glass carries what part of a 5000 N tensile load ?