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A temperature measurement system has the following specifications: -128 to 781°C Range Linearity error 0.29% FSO Hysteresis error 0.12% FSO Sensitivity error 0.04% FSO Zero drift 0.32% FSO FSO stands for "Full Scale Output". Estimate the overall instrument uncertainty for this system based on the available information. Use the maximum possible output range over the FSO in your computations.

Dynamics of Rigid Bodies Please help ASAP. Rate will be given accordingly. Please answer correctly this is my last chance. Please write your answer on paper. Thank you so much. Note: The tolerance is ±1 in the third significant digit.

The endurance limit for a material is found by rotating beam specimen test to be S,' = 52 kpsi. Using a reliability estimate of 99.9 percent, estimate the endurance limit if the material is to be placed in reversed axial loading. Table 6-4 Reliability Factors k, Corresponding to 8 Percent Standard Deviation of the Endurance Limit Reliability, % Transformation Variate z. Reliability Factor k, 50 1.000 90 1.288 0.897 95 1.645 0.868 99 2.326 0.814 99.9 3.091 0.753 99.99 3.719 0.702

DEPARTMENT OF MECHANICAL ENGINEERINGMENG 303 PRINCIPLES OF COMPUTER AIDED ENGINEERING Failure mode and effect analysis for Autonomous underwater vehicles, based on any standard.   plese dont late

Which of these statements are correct?

Please show work for practice problem 12

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Please fast. This is mechanical engineering Problem (Operation research )

The shear modulus, G, of a material can be determined by applying a torque, T, on a cylindrical material specimen and measuring the angular twist, 0. The modulus can then be calculated from: G the specimen radius and length, respectively, The relative uncertainty in each measured variable (L. T, t. 0. R) is + 3.7% 3LT where R and L are %3D 2 Ree What is the total relative uncertainty in G?

(j) In GD&T, geometric features can be characterised using . material condition modifiers symbols and interpretation datums O tolerance zone

Problem (1): Determine tolerance value and limit dimension of the rod which a diameter is ∅44 mm (nominal size), according to the e7 limit deviation (∅44e7). es=-50 mkm, ei=-75 mkm. Determine the basic size, tolerance and limit dimensions.

C Dynamic Analysis and Aeroelasticity SECTION B Answer TWO questions from this section ENG2012-N The moment of inertia of a helicopter's rotor is 320kg. m². The rotor starts from rest and at t = 0, the pilot begins by advancing the throttle so that the torque exerted on the rotor by the engine (in N.m) is modelled by as a function of time (in seconds) by T = 250t. a) How long does it take the rotor to turn ten revolutions? b) What is the rotor's angular velocity (in RPM) when it has turned ten revolutions?

Home work for tensile test The following data was obtained from a tensile test on 135 Load (kN) Extension (mm) 16 32 56 72 95 110 132 142 140 0.2 0.4 0.7 0.9 1.5 2.5 5.0 8.5 10.0 12.0 a specimen of 10mm diameter and gauge length 60mm. Using the graph paper supplied, plot the load-extension diagram and determine: (1) The tensile strength (2) 0.1% Proof Stress (3) Young's Modulus for the specimen

The following data were collected from a 12 mm diameter test specimen of Magnesium. LOAD (N) GAUEGE LENGTH (mm) 0 5000 10000 15000 20000 25000 26500 27000 26500 30.000 25000 30.0296 30.0592 30.0888 30.15 30.51 30.90 31.50 (maximum load) 32.10 32.79 (fracture) After the fracture, the gauge length is 32.61 mm and the diameter is 11.74 mm. a) What is the elastic modulus? b) Percent elongation at fracture? c) Percent elongation after fracture? d) What is the Poisson's ratio? e)Draw the engineering stress-strain diagram corresponding to the values in the table. Call this plot I. Now consider this experiment is repeated at a higher temperature with an identical sample. Draw the new engineering stress-strain diagram, call it plot II and highlight the differences (on the same graph) between I and II.

Problem (7): Determine tolerance value and limit dimension of the rod which a diameter is ∅25 mm, according to the H9 limit deviation (∅25H9). ES=-12.7 mkm, Eİ=+0 mkm. Determine the basic size, tolerance and limit dimensions.

mathlab code: %Press-Fit Example Problem 117 %Steel, psi ES=30*10^6 MuS=0.292; %Cast Iron EC=14.5*10^6; MuC=0.211; di=0; d0=2.002; Di=2.000; D0=3.000; % tolerance tol=d0-D0; % Pressure Eq. (3-56) R=Di/2; r0=D0/2; ri=di/2; Hub=(1/ES)*((r0^2+R^2)/(r0^2-R^2)+MuS);     Inner=(1/EC)*((R^2+ri^2)/(R^2-ri^2)-MuC);    p=tol/(R*(Hub+Inner))

Problem 6-5: The mass of a test specimen of metal alloy is measured to be m = 674.4 g. The procedure has a standard uncertainty of 1.0 g. The volume of the specimen is measured to be V = 261.1 mL with an estimated standard uncertainty of 0.1 mL. Estimate the density of the specimen and its uncertainty.

cience ourses / MENG286-01 2020-211 / Final Exam Final Exam Primary Creep: slope (creep rate) decreases with time ered f2.00 Select one: jon True False

Chapter 3: 13. What type of geometric tolerance has no datum features? 14. A theoretically exact dimension is called a 15. The feature symbol specifies that a group of two or more interrupted features of size are to be considered one single feature of size. 16. For an individual regular feature of size, no element of the feature shall extend beyond the maximum material condition boundary (envelope) of perfect form. This statement is the essence of 17. What is the name of the symbol used to identify physical features of a part as a datum feature and must not be applied to centerlines, center planes, or axes? 18. The is the condition in which a feature of size contains the maximum amount of material within the stated limits of size. 19. The total positional tolerance equals the sum of the tolerance and the tolerance.

A light bulb manufacturer wants to maximize bulb lifetime. Four parameters are to be tested: Parameters a and b are the concentrations of a certain alloys in the filament. Parameters c and d are the temperature and speed, respectively, at which the filaments are extruded in the manufacturing process. A three-level experiment is be used. Levels 1, 2, and 3 correspond to low, medium, and high values of each respective parameter. Taguchi's 9-run design array (as in the learning module) is to be used. For each experimental run, thirty bulbs are tested, and the mean time to failure (MTTF) for each run is recorded as X₁, X₂, etc. These values, in order, are 1318, 1375, 1414, 1490, 1532, 1296, 1455, 1219, and 1266 hours, to four significant digits. (a) Generate a table with the above values configured as a Taguchi 9-run design array (Excel is recommended). Calculate all 12 level averages, i.e. Xal, Xa2, X3, Xb₁‚ õ2, Xd3 (b) Generate four plots, showing the dependence of X on each parameter.…

A force measurement system (weight scale) has the following specifications as shown in Table 1: Estimate the overall instrument uncertainty for this system based on available information. FSO refers to full-scale operating range.

Mechanical Engineering xyz= 703 Stress, ksi (log) 72 49 35 28 10³ 8 x 10³1 10¹ 401 X 8't 49 ksi 10 ksi 401 X 9'1 35 ksi 28 ksi 105 Cycles (log) 106 19.8 The provided S-N curve shows the fatigue strength of a ferrous component with unknown geometry. 107 Given the following duty record, how much life is consumed at each stress level? 60 ksi 500 cycles 2000 cycles (600 000 + XYZ*100) cycles (15000 + XYZ) cycles 40000 cycles

13. The presence of a defect in the material illustrated in the figure (http://aero.tu sofia.bg/~vlados/ae2test04.png) was determined using: 109 omniscan TEEN TEL 000 2419 IN EV O Eddy current testing. O Radiography testing. O visual testing. Ultrasonic testing. KAU 1919 0:4 45 A

1. On the drawing attached, before any geometric controls are applied, what is the coaxility tolerance that is implied between the diameters?

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zain 10 2G 3G zain IQ Z Questions of Lectu... -> Questions of Lecture Five: Q1)) Define the following: 1) The stress & the strain 2) Mechanical stress and mechanical strain 3) yield strength and tensile strength 4) Modulus ofelasticity and the strain hardening Q2)) Fill the following blanks: 1)) Tensile tests are used to 3)) The most application tests of applied static stresses to which materials can be subjected are ---------, ---------, --------- 4)) Tensile stresses cause ---------, and compressive stresses ----------, while shear stresses ----------, of the material. 5)) Engineering stress-strain is important in ----------, while the true stress-strain is important in ---------- 6)) The unit of mechanical stress is --------- or ----------, while the unit of strain is n compression test, when specimen is compressed, its height is ---------, and its cross-sectional area is 8)) Compression is in contrast to the tensile, the compression test contributes to the ----------, in stress…