201_HW_4

W Determine the transformed reduced stiffness matrix for a unidirectional ply oriented at 45 degrees to the global x-axis for the material. S [Q]= [150.72 2.41 2.41 8.04 0 0 English (United Kingdom) Text Predictions: On - Q Search 23 Where: Using the formula below: F3 E [T] = $ 4 € R [T]-¹= F 0 0 GP F5 10] [cos²0 sin²0 -sin cose Accessibility: Good to go % 5 [cos²0 sin²0 sin cose Q = [T]¹[Q][T] T T F6 6 G sin²0 cos²0 sin cose sin 20 cos²0 -sin@cose 2sin cose -2sin@cose cos²0-sin²0] & H -2sin cose 2sin cose cos²0-sin²0] FB LU U * 00 O J F9 8 ( 9 F10 K M Focus GO F11 0 B P

Problem 1: (50 points) In Avengers 2, Captain America's improved shield is made from unobtainium, a new material that will soon be available in a store near you. Unobtainium has the normal stress- strain diagram shown. The proportional limit, the elastic limit and the yield point are identical in this material. o [MPa] 2001 175 150 125 100 Fig.1 Normal stress-strain 75 50 25 0 0. 0.05 0.1 0.15 0.2 0.25 Unobtainium has a Poisson's ratio of 0.3. a. [6pts] Identify the yield point oy, the ultimate stress ou and the fracture stress of. Include units. c. [25pts] A bar of unobtainium has a length of 1.5 m, a width of 100mm and a height of 50 mm, as shown. The cross-sectional area is 50mm 100mm = 5 x 10-³m². The bar is subjected to an axial force of 375 kN. Find the normal stress in a cross-section of the bar. b. [5pts] How do you find Young's modulus from this graph? Find its value with units. whesta fins dus al hoss P = 375 KN 1.5 m 0.3 50 mm 100 mm & [mm/mm] Is the material within its…

HEAT TRANSFER CASE:  I want to know what temperature in (°F) the cylinder will have inside. It's a heat transfer problem. what is T2 ? HEAT TRANSFER They gave me an answer all squashed together that i can't make sense of it. If you could help me makes sense of it thank you!

Second m oment of area of a section: With respect to the x axis: I [[ v²dxdy D 8. A plate is bounded by the positive x and y axes and the curve y=3-\x . Find the second moment of area of the plate with respect to the x-axis. [ANS : 8.1]

Review the Outpatient Clinic Case 410057 in AHIMA VLab, which can be found in Authentic Patient Cases. After reviewing this case, review the code assignments that were made by the encoder in the table below. Code Assignment Code DescriptionAdmitting Diagnosis C50.312 Malignant neoplasm of lower-inner quadrant of left female breastSecondary Diagnosis or DiagnosesZ17.1 Estrogen Receptor negative statusPrincipal Procedure 19301-RT Partial MastectomySecondary Procedure 19285-RT Placement of breast localization device, percutaneous; first lesion, including ultrasound guidance (RT- Right side of the body)Third Procedure 14301 Adjustment tissue transfer/rearrangement Now determine whether or not the diagnosis/diagnoses show medical necessity for the procedures performed. Explain your answers in detail in the boxes below.

Help with #3 and coding in MATLAB

permanent-magnet (pm) genera x Bb Blackboard Learn L STAND-ALONE.mp4 - Google Dri x O Google Drive: ülwgjuó jc lis u O ME526-WindEnergy-L25-Shuja.p x O File | C:/Users/Administrator/Desktop/KFUPM%20Term%232/ME526/ME526-WindEnergy-L25-Shuja.pdf (D Page view A Read aloud T) Add text V Draw Y Highlight O Erase 17 of 26 Wind Farms Consider the arrangement of three wind turbines in the following schematic in which wind turbine C is in the wakes of turbines A and B. Given the following: - Uo = 12 m/s A -XẠC = 500 m -XBC = 200 m - z = 60 m - Zo = 0.3 m U. -r, = 20 m B - CT = 0.88 Compute the total velocity deficit, udef(C) and the velocity at wind turbine C, namely Vc. Activate Windows Go to Settings to activate Windows. Wind Farms (Example Answer) 5:43 PM A 4)) ENG 5/3/2022 I!

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I need help with my MATLAB code. I am trying to plot the semi major axis and eccentricity with the following code with rungge kutta method. I have two different nnn's in the code which produce two different step sizes. So, I am wondering why both give the same exact plots for semi-major axis and eccentricity. The orbital dynamics fucntion considers J2, drag, SRP, and third body effects.   % Orbital elements obtained from TLE inc = 63.5000118; % Inclination (degs) raan = 19.999977; % RAAN (degs) ecc = 0.001; % Eccentricity argp = 120.02165342; % argument of perigee (degs) v = 0; % True anomaly (degs)   a = 6584.697271; % Semi-major axis (km)   mu = 3.986e5; period = (2*pi*sqrt((a^3)/mu));     % Calculating the state vector in eci frame [x, y, z, vx, vy, vz] = kep2cart(a, ecc, inc, raan, argp, v); Y = [x, y, z, vx, vy, vz];   options = odeset('RelTol', 1e-12, 'AbsTol', 1e-12);   nnn1 = 800; t_step1 = period/nnn1; m6 = 50; h_step6 = t_step1/m6; t_total6 = 0:h_step6:10*period;   [t6,…

Solve the problem correctly in a handwritten format. Strictly chatgpt not allowed Mechanical engineering

K mylabmastering.pearson.com Chapter 12 - Lecture Notes.pptx: (MAE 272-01) (SP25) DY... P Pearson MyLab and Mastering Mastering Engineering Back to my courses Course Home Scores Course Home

***Is not an exam or test . Is a homework I just want to see the resolution

I need help solving this problem.