5AL Lab 3 Assignment Submission Template - F23 (1)

help!Options:1: Roller at D / Pulley2: Zero / two / multi3: Force / Direction4: B / F / E

5 of 6 (4 complete) HW Sc ic) se More Info on he en F=0.075x F=0.035x F=0,020x Spring #1 Spring #2 A Spring #3 Elongation (x) [mm] Print Done Clear Air Force (F) [N]

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 :

help with the question pls

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

Options are "angle of twist" and "rotation angle"

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

Find the characteristic frequencies and the characteristic modes of vibration for systems of masses and springs as in Figure 12.1 and Examples 3, 4, and 6 for the following arrays. 14. k, m, 2k, m, k 5k, m, 2k, m, 2k 15.

Match the appropriate velocity of the cannon ball at the time frames if the cannon ball was shot out with an initial velocity of 50m/s. OB DO E A Choose ] В [ Choose ] C [ Choose ] D [ Choose ] E [ Choose ] > >

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

help please!!

6 6 - A) -22.124 j NmB) (-22.124) k NmC) (-42.124) i NmD) (-12.124) i NmE) (-32.124) j Nm

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,…

6cm I 3em Icm <- Scr ]] Icm

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)

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

Show all steps and formulas

13. User tool frame UT[3] was set up by the programmer with three-point method for UT setup provided by FANỤC robot system. Which of the following statements is correct. (a) UT[3] frame is measured relative to UF[h] frame. (b) The orientation of UT[3] frame is the same as the orientation of default TCP frame (i.e. Def- TCP frame). (c) The origin of UT[3] frame is exactly aligned to the origin of default Def-TCP frame. 14. Using three-point method for user tool frame UT[k] setup, a robot programmer can set up the user- defined of UT[k] for an end-effector. (a) position (i.e. origin) (b) orientation (c) position (i.e. origin) and orientation

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

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