A03-Questions-1

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

kamihq.com/web/viewer.html?state%=D%7B"ids"%3A%5B"1vSrSXbH_6clkKyVVKKAtzZb_GOMRwrCG"%5D%... lasses Gmail Copy of mom it for.. Маps OGOld Telephone Ima. Preview attachmen... Kami Uploads ► Sylvanus Gator - Mechanical Advantage Practice Sheet.pdf rec Times New Roman 14px 1.5pt BIUSA A Xa x* 三三 To find the Mechanical Advantage of ANY simple machine when given the force, use MA = R/E. 1. An Effort force of 30N is appliled to a screwdriver to pry the lid off of a can of paint. The screwdriver applies 90N of force to the lid. What is the MA of the screwdriver? MA =

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I need help solving this problem.

I want the answer of part c

4. Documents business requirements use-case narratives.for only one process note:  please  i want Documents like this in pic

Don't copy paste someone else answer if I get to know I'll report and downvote too do on your own and only handwritten with proper steps not that handwritten only

Hartley Electronics, Inc., in Nashville, producesshort runs of custom airwave scanners for the defense industry.The owner, Janet Hartley, has asked you to reduce inventory byintroducing a kanban system. After several hours of analysis, youdevelop the following data for scanner connectors used in onework cell. How many kanbans do you need for this connector?Daily demand 1,000 connectorsLead time 2 daysSafety stock 12 dayKanban size 500 connectors

I need handwritten solution with sketches for each

Hello I'm having trouble with this assignment, I don't understand how the plot function works for ordered pairs. I undertand that the points of the line would be the origin(0,0) and (x = cos(theta) . y = sin(theta)).

You are assigned as the head of the engineering team to work on selecting the right-sized blower that will go on your new line of hybrid vehicles.The fan circulates the warm air on the inside of the windshield to stop condensation of water vapor and allow for maximum visibility during wintertime (see images). You have been provided with some info. and are asked to pick from the bottom table, the right model number(s) that will satisfy the requirement. Your car is equipped with a fan blower setting that allow you to choose between speeds 0, 1,2 and 3. Variation of the convection heat transfer coefficient is dependent upon multiple factors, including the size and the blower configuration.You can only use the following parameters:

+ → CO A student.masteryconnect.com/?iv%3D_n5SY3Pv5S17e01Piby Gr 8 Sci Bench 1 GradeCam Rutherford TN 2021 AHMAD, ASHNA D0 3 of 35 A student develops a model of an electric motor using two pins, a wire coil, coil continues to spin with a certain speed. wire coil pins magnet tape battery How can the student increase the speed of the electric motor? O by using wider pins O by using thinner pins O by using less wire in the clil O by using more wire in the coil e Type here to search 近

I need help coding in MATLAB. I have a .txt file containing the following data. That data is saved in a file named data.txt. I am wondering how I could extract all or some of that data into another .m file. Can you show me the code.   [[5.0018696581196584, 17.863820207570207, -13.086858974358975], [5.0018696581196584, 17.863820207570207, -13.086858974358975], [5.0018696581196584, 17.863820207570207, -13.086858974358975]]

I am having trouble with the folloiwng MATLAB code. I am getting an error that says "unrecognized function or variable 'numericalPropogatorOptions". I have the aerospace toolbox and the aerospace blockset added. what add on do I have to download to use that function. How do I make this code work?     % Define Keplerian Elements a = 29599.8; e = 0.0001; i = 0.9774; Omega = 1.3549; w = 0; M = 0.2645; [RECI, VECI] = Kepler2RV(a, e, i, Omega, w, M); initialState = [RECI * 1e3; VECI * 1e3]; % Initial position (m) and velocity (m/s)   % Define constants mu = 3.986004418e14; % Gravitational constant (m^3/s^2) earthRadius = 6378.1363 * 1e3; % Earth radius in meters j2 = 1.08263e-3; % J2 perturbation coefficient   % Define propagator options propOptions = numericalPropagatorOptions('CentralBody', 'Earth', ... 'GravitationalParameter', mu, ... 'InitialState', initialState, ... 'OutputTimeStep', 300); % Output every 300 seconds   % Add perturbations addGravityModel(propOptions, 'Degree', 2,…

I need help with the first part and Matlab for this problem