- 1:16ت تم مشاركة العرض من جاندJanada 29,器AnnotateEdit POFQ m AA ..InsertPensA ANote 7 Mar 2021 at 11 64 30 AMVNmotoniarEx Some non- Nawtonion luds behave asa Bugham Plastie forwhich shear strass Can be exprassed = Ly + - forbaminor Rlowoba Bingham plastic in athe valocily prokle given aswhare in the Gonstant pressure drop along thehonizontalgipaf radius R,R),(r-Jengthy A is tedynamic viscos:tirisProm tha canter lina, and is the iebd.strass.Determine ca) the shear stress atah pipe wadistancab) the dnag force actingon a pipe seetionof h L.Selutiona fó3p7xpy3dيلم التقديم الآن بواسطة عامر حميد مجيد

Name: - 1:16ت تم مشاركة العرض من جاندJanada 29,器AnnotateEdit POFQ m AA ..In
Uploaded: 2024-03-20T06:56:55.000Z
Channel: Bartleby
Description: - 1:16ت تم مشاركة العرض من جاندJanada 29,器AnnotateEdit POFQ m AA ..InsertPensA ANote 7 Mar 2021 at 11 64 30 AMVNmotoniarEx Some non- Nawtonion luds behave asa Bugham Plastie forwhich shear strass Can be exprassed = Ly + - forbaminor Rlowoba Bingham

Write the given value using suitable variables. Here u(r) signifies velocity profile and τ…

Engineering

Mechanical Engineering

Ex Some non- Nawtonion luds behave asa Bnghawn plastic for which shear stress can be expratsed = Ly + - for baminor Rlowoba Bingham plastic in a honizontalgipaf radius R, the valocih pofle where is ths constant pressure diop along Hhe pipe qar lengthy is the olyma from tha canter lina, cand is the iebd stress. Determina ca) the shear stress att pipe Ca giclen as Ur- reRY+(r-R), wnit mic viscosity, isthe radial distance eb) the drag forrea acting on a pipe santion of hagh L. . Salution

Ex Some non- Nawtonion luds behave asa Bnghawn plastic for which shear stress can be expratsed = Ly + - for baminor Rlowoba Bingham plastic in a honizontalgipaf radius R, the valocih pofle where is ths constant pressure diop along Hhe pipe qar lengthy is the olyma from tha canter lina, cand is the iebd stress. Determina ca) the shear stress att pipe Ca giclen as Ur- reRY+(r-R), wnit mic viscosity, isthe radial distance eb) the drag forrea acting on a pipe santion of hagh L. . Salution

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

M13.6 Principal stresses from rosette data scenes -200 µE 23 Eb = 200 με Ec 500 µE 30° 30° Ex (LE) a Ey (µE) Yxy (Lurad) The strain rosette shown was used to obtain normal strain data at a point on the free surface of a steel (E = 200 GPa; v = 0.32) plate. Op1 (MPa) Determine the normal strains, the shear strain, and the principal stresses in the x-y plane. Op2 (MPa) Try One 1st 2nd 3rd attempt enter
where the normal stress is of ox , Oy Q3: A state of plane stress case and txy shown in fig. At a clockwise angle of 30 ° the normal stress is 5 MPa (compression) and it is 4 MPA at an angle of 50 ° in tension. Find the maximum shear stress. y Txy 0,=8 MPa X
Need Solution through 15min
Please help me with #4 of this problem. Thank you!
A slender rod is k= 160m10* 320MPa Subjected to tenston, the lood is inceeased (MP) incrementally and the 320 plot at left isobtined. * What can be said for ultimate stronpth? 0.004 0.002 *If the loading is kept until to o iš 320MPA withdrawn, *The vaterial which the rod is node of, is a duc tile noteniel, explain why? ond suddenly what will Be the permanent stroin ? * If the looding ás ceoscd at some louel and is ceoscod at some lovel and the rod is released and Eenp lengineering strain) Come out to be 0,003, what will be the Correspen deny true stran (E)?
Please it in details and don't copy old solution
I need the answer as soon as possible
answer as soon as possible
QI/ for the vessel pressure shown in fig find longitudinal and hoop tensile stress in the wall knowing that internal pressure is 2.5 MPa and thickness of the wall Smm R-1m L-2m
Please don't provide handwritten solution .....
View Policies Current Attempt in Progress Consider a point in a structural member that is subjected to plane stress. Normal and shear stress magnitudes acting on horizontal and vertical planes at the polnt are S-39 MPa, 5,- 17 MPa, and Sy-31 MPa. (a) Determine the principal stresses (opl > o2) and the maximum in-plane shear stress rmax acting at the point. (b) Find the smallest rotation angle 0, (counterdockwise is positive, dockwise is negative) that will rotate to prindpal directions. Then show these stresses in an appropriate sketch (e.g see Figure 12.15 or Figure 1216) Answers: MPa. MPa. MPa Tmax = 0, = Attempts: 0 of1 used Submit Answer Save for LatAr
Question 3 of 15 View Pollcies Current Attempt in Progress Consider a polnt in a structural member that is subjected to plane stress.Normal and shear' stress magnitudes acting on horizontal and vertical planes at the point are S, -39 MPa. 5,- 17 MPa, and Sy-31 MPa. (a) Determine the prindpal stresses (op1 > Op2) and the maximum in-plane shear stress Tmax acting at the point. (b) Find the smallest rotation angle 0, (counterdockwise is positive, dockwise Is negative) that will rotate to principal directions. Then show these stres ses in an appropriate sketch (eg. see Figure 12.15 or Figure 12.16) Answers: MPa. MPa. MPa Toas = 0, = Attempts: 0 of 1 used Submit Anwer SaIL FOr Latu