LAB 4 Table 2 Section G11

Find a state space representation of the network shown below when the output is the displacement on mt. Let my = 2 kg, m₁ = 4kg, F = 10 N, b₁ = 1 Ns/m, b2 = 2 Ns/m, k₁ = 2 N/m, and k2 = 4 N/m, Force of material placed in truck bed C7 Truck vehicle mass Shock absorber A Tire Select the correct response: [dx₁ dt 0 0 10 dx₂ 00 1 24 1 dt X₂ Xour][0 1 0 0] +F dv at ww dx₁ at dx- dt du dt du dt 10 1112 10 POIN VI [ou]= [0 1 0 0] NIW

4-6- SI A six-liter, eight-cylinder, four- Stroke cycle race car engine operates at 6000 RPM using stoichio- metric nitromethane as fuel. Combustion efficiency. is 99%, and the fuel input rate is 0.198 kg/see. a- Volumetric efficiency of the engine [!] b-Flow rate of air into the engine. [ kg/sec.:] Calculate :

A B C D E Match the process, positions, and parts of an internal combustion engine using the figure. G H [7] C K A D B ✓ [Choose ] Exhaust valve Compression stroke Intake stroke Bottom Dead Center (BDC) Intake valve Combustion Chamber Combustion/Power stroke Piston Top Dead Center (TDC) Exhaust stroke [Choose ] [Choose ] E F

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,…

A local camera station is tracking a UFO sigbting in the evening aky, Find the velocity and acceleration of the UFO in the r and theta directions and then find the velocity and acceleration in the x and y directions. 30 043 [rad/sec] +.004308 [rad/sce"] 6000 [ft] 283 [f/sec] 12.011 [f/sec] e (heta dot) Y axis X axis

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Solve this question pl

On drawing 31A063, how many holes are specified?   All abbreviations are standard

On drawing 31A063, what is dimension F in mm?   All abbreviations are standard

Build the pneumatic circuit in the following pneumatic sequence using the cascade method: [A- B-] [C+ D- A+] [C- B+ D+]

Build the pneumatic circuit in the following pneumatic sequence using the cascade method: [A+ B+] [A- B- C+ A+] [B+ A- B- C-]

A particle is subjected to the action of two forces: F1 = 4 i+7j+7 k [kN] and F2 = 5 i - 6 j - 5 k [kN]. The coordinate direction angle of the resultant force with X-axis is: Select one: a. ar = 83.81° b. ar = 31.93° C. Ar = 13.93° O d. ar = 166.07°

F3 Ⓡ Zaxis 9 54 F2 fi хакд yax.s ANO) D.Mart Co moz Ctiven: Take all vectors to have a magnitude of 11.1 [KM] Q₁ has angle 17° 21 2001 200 7 62 has angle 75° wa The hoteles 40 Add all the vectors together, what is the magnitude of resultant vector ? 34

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

In the Blasius equation stream function: j is a dímensionless plane p(x, y) f(n) VDUX Values of f are not given in Table 7.1, but one published value is f(2.0) = 0.6500. Consider airflow at 6 m/s, 20°C, and 1 atm past a flat plate. Atx= 1 m, estimate (a) the height y; (b) the velocity, and (c) the stream function at 7= 2.0.