Can you explain the algebra steps that aren't shown but stated to be there, on how to get this equation Sowewent Tog({BN]) =Recall ez. (3.98)maxomize:n2WKk=12B ₁T [ B N ] ~ V KB+B-B₂-B2(B₁₂+ Boß3)[BN]= 2(BB₂- Boß³) B - B²₁ + B¾ - B²³2(B1B3+ Boẞ2)in termsTwecan re-write06و* = (Bo, B., B2, B3)"Aftersame algebraدwe SeeT} ( {EN]) = g(B) = }} [K] B2(B1B3 - Boẞ2)2 (B₂B3 + Boß₁)

Answered: Image /qna-images/answer/25950122-f152-46fd-b523-08aecfb8ca6b.jpg

Answered: So we went To g({BN]) = Recall ez.…

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

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I need help with a MATLAB code. I need to find two values of n, one that is positive and one that is negative, that will give all negative real roots. Can you help me find them? function [r] = find_roots(n) % Define constants I = 400; J = 150; x = (J/I) - 1; y = n - 1; Q = y + x*(y-1); % Define the coefficients of the quadratic equation coefficients = [1, 0, (3*x+Q^2+1), 0, (3*x*Q+Q^2)]; % Find the roots r = roots(coefficients); end
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I need help with my MATLAB code. There is an error in the following code. The error says my orbitaldynamics function must return a column vector. Can you help me fix it? I tried changing the semi colon to a comma in dstate_dt = [v, a_total]; but it still gives me error mu_earth = 398600.4418; % Earth's gravitational parameter (km^3/s^2) R_earth = 6378.137; % Earth's radius (km) C_d = 0.3; % Drag coefficient (assumed) A = 0.023; % Cross-sectional area of ISS (km^2) m = 420000; % Mass of ISS (kg) % Initial conditions: position and velocity (ISS state vector) % ISS initial state vector (km and km/s) - sample data state_ISS =[-2.1195e+03, 3.9866e+03, 5.0692e+03, -5.3489, -5.1772, 1.8324]; % Time span for 10 revolutions T_orbit = 2 * pi * sqrt((norm(state_ISS(1:3))^3) / mu_earth); time_span = [0, 10 * T_orbit]; % Step 3: Numerical integration using ODE solver options = odeset('RelTol', 1e-12, 'AbsTol', 1e-12); [t, state] = ode45(@orbitalDynamics, time_span, state_ISS,…
Don't Use Chat GPT Will Upvote And Give Handwritten Solution Please
хоос» 0 Python 3 (p Define a python function to determine the 2nd moment of area I, under the parabola, with respect to the centroidal-axis. The parabolic curve is defined as z = ky2, where k = b/h². The centroidal axis has a given distance d with respect to z axis. Hints: Use the parallel axis theorem. Find the 2nd moment of area against z axis first and then use the formula I₂ = I₁ + d²A to calculate I, where d is a given value (no need to derive). Note that this question requires you to derive the equation first. $ 4 l) | Idle Mem: 260.77/12288.00 MB Q F4 R y 1 1 0 do 5 [ ]: # Complete the function given the variables b,h,d and return the value as "Area","Iz" and "Ic" # This is not about numerical integration, we only need the analytical solution. # Don't change the predefined content, only fill your code in the region "YOUR CODE" Mode: Command % 9 F5 0 T . Markdown v z = ky² 2 6 C F6 Validate Y & 7 8: F7 U * 8 DII F8 I 19 F9 b O ) Ln 1, Col 1 English (United States)…
A member of your team gives you the following MATLAB program. Your job is to create the function used in the program. H = 30; % height [cm] V = 50; % volume [cm^3] % calculates the radius [cm] of a cone R2 = RadiusCone(H,V);
A bar is pinned to ground at its O with the bar rotating clock-wise at a constant rate of Ω=8.9[rad/s]. Block P is traveling to the left along a straight path towards with a constant speed of vp=9.7 [ft/s]. Given that h=4.7[ft] and rA/O=1.2[ft], solve the following: What is the J^ component of v¯A? What is the J^ component of (v¯P/A)rel? What is the I^ component of (v¯P/A)rel? What is the ω of the local coordinate system (this is the ω in the relative velocity and acceleration equations.
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४ B: Find the numerical solution for the 2D equation below and calculate the temperature values for each grid point shown in Fig. 2 (show all steps). (Do only one trail using following initial values and show the final matrix) [T1] T₂ T3 [T] 1 = [0] 0 0 d dx dx) (ka)+4(ka) = dy -20xy, k = 1 + 0.3 T ge L=3cm, 4x= Ay B.Cs.: at x=0=LT=0°C at y=0-L T=10°C Fig. (2)
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1. Draw the shear force diagram for the system below. 50 [kN] 48 [kN] 5 [m] 10 [m] 3[m] 7.5 [m] 3[m]
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