Phonation Lab

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!

I need help in my MATLAB code. The following code gives me the plot in the image. How do I answer the question "Running the program the region around the object detection is cropped out. Estimate the background in that region."   % Constants   MU_E = 398600.4418; %[km3 s-2], gravitational parameter R_E = 6378.137; %[km] mean earth radius omega_E = [0;0;7.2921150e-5]; %[rad s-1] rotation rate of Earth   % Telescope information: lat = 32.903342; %[deg] site latitude lon = -105.529344; %[deg] site longitude alt = 2.225; %[km] site altitude above sea level   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % Load a FITS image   fname = '00095337.fit'; fInfo = fitsinfo(fname); img = fitsread(fname);   % Crop the image to show just the object: img_cropped = img(1980:2030,1720:1780);   % Load the labeled image img_labeled = imread('00095337_labeled_stars.png'); img_labeled = img_labeled(102:863,605:1363,:);   % Get rid of "hot" pixels (cosmic rays, disfunctional…

Part III Capstone Problem Interactive Physics - [Lab7Part3.IP] Eile Edit World View Object Define Measure Script Window Help Run StoplI Reset 圖|& 品凸? Time Length of Spring 22 6.00 dx Center of Mass of Rectangle 2 5.000 Tension of Rope 3 Jain@ IFI ... N ot rot ***lad Split 4.000 Velocity of Center of Mass of Rectangle 2 Vx Vx V Vy MM Ve - m/s m/s 3.00 *** m/s Vo ..* lad/s 2 00 Center of Mass of Rectangle 1 1.000 tol rot *.* rad EVelocity of Center of Mass of Rectangle 1 Vx Vx VVy M 0.000 -m/s w 30 m/s w.. MI Ve 母100 *** m/s Vo ... rad/s + EAcceleration of Center of Mass of Rectangle 1 Ax Ax A Ay AUJAI Ae --- m/s^2 ... m/s^2 -- m/s^2 .-- rad/s^2 3.00 Aø Mass M1 = 2.25 kg is at the end of a rope that is 2.00 m in length. The initial angle with respect to the vertical is 60.0° and M1 is initially at rest. Mass M1 is released and strikes M2 = 4.50 kg exactly horizontally. The collision is elastic. After collision, mass M2 is moving on a frictionless surface, but runs into a rough patch 2.00…

HW_5_01P.pdf PDF File | C:/Users/Esther/Downloads/HW_5_01P.pdf 2 Would you like to set Microsoft Edge as your default browser? Set as default To be most productive with Microsoft Edge, finish setting up your Complete setup Maybe later browser. (D Page view A Read aloud V Draw 7 Highlight 2 of 3 Erase 5. Two cables are tied to the 2.0 kg ball shown below. The ball revolves in a horizontal circle at constant speed. (Hint: You will need to use some geometry and properties of triangles and their angles!) 60° 1.0 m 60° © 2013 Pearson Education, Inc. (a) For what speed is the tension the same in both cables? (b) What is the tension? 2. 2:04 PM O Type here to search C A 2/9/2021 (8)

I need help solving this problem.

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]]

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 ] > >

Given: Mass = M, Radius = R, Moment of Inertia = I, Distance =  H, Gravity = g, Initial timing = 0 Unknown =  How long will the [delta t] process take? (time) Please keep in mind that almost every variable is unknown! We are given no numbers and are instructed to generate a solution using the variables [ "R, M, g, I and H." ]  Target =  Find an equation that, if we could substitute numbers, would determine how long the process would take.  Newton's second law and torque seem to be relevant based on how the problem is written. * Also please show drawing based on what we are calculating

Please examine how you got answer step by step please

For the Following question Graph all 4 : [I just need all 4 graphs and please explain and make clean solution] Position vs time Velocity vs time Acceleration vs time Force vs time [For your convenience, I have solved the numerical solutions for the problem] (Please Look at the picture since it is much cleaner) Question : A 550 kilogram mass initially at rest acted upon by a force of F(t) = 50et Newtons. What are the acceleration, speed, and displacement of the mass at  t = 4 second ? a =(50 e^t)/(550 ) [N/kg] v = ∫_0^t▒(50 e^t )dt/(550 )= v_0  +(50 e^t-50)/550=((e^t- 1))/11 x = ∫_0^t▒(e^t- 1)dt/(11 )= x_0  +(e^t- t - 1)/(11 ) a(4s)=(50*54.6)/550= 4.96[m/s^2 ] v(4s)=((e^4-1))/11= 4.87[m/s] x(4s)=((e^4- 4 - 1))/11= 4.51 [m]

Study Area Document Sharing User Settings Access Pearson mylabmastering.pearson.com P Pearson MyLab and Mastering The crash cushion for a highway barrier consists of a nest of barrels filled with an impact-absorbing material. The barrier stopping force is measured versus the vehicle penetration into the barrier. (Figure 1) Part A P Course Home b My Questions | bartleby Review Determine the distance a car having a weight of 4000 lb will penetrate the barrier if it is originally traveling at 55 ft/s when it strikes the first barrel. Express your answer to three significant figures and include the appropriate units. Figure 1 of 1 36 μΑ S = Value Units Submit Request Answer Provide Feedback ? Next >

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,…

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

Help solve this USING MATLAB

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

I was given a practice question for transforming equation. In the image I will have a slide the lecture note of an example of it being done but I do not understand what was done exactly. Please explain how to answer the question. Thank you

Access Pearson Study Area mylabmastering.pearson.com P Pearson MyLab and Mastering Document Sharing User Settings The car in (Figure 1) having a mass of 2 Mg is originally traveling at 2 m/s. Assume 0 = 22°. Figure 1 of 1 Part A P Course Home b My Questions | bartleby ■Review Determine the distance it must be towed by a force F = 4 kN in order to attain a speed of 6 m/s. Neglect friction and the mass of the wheels. Express your answer to three significant figures and include the appropriate units. Α ? S = Value Units Submit Request Answer Provide Feedback Next >

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)…

I need help in the following MATLAB code. How do I add the code to answer the following question "Do you find more object detections in the image than the one that is cropped out? Explain how you would discriminate that from a dead pixel, a hot pixel, or a cosmic ray event."   fname = '00095337.fit'; fInfo = fitsinfo(fname); img = fitsread(fname);   % Crop the image to show just the object: img_cropped = img(1980:2030,1720:1780);   % Load the labeled image img_labeled = imread('00095337_labeled_stars.png'); img_labeled = img_labeled(102:863,605:1363,:);   % Get rid of "hot" pixels (cosmic rays, disfunctional pixels) max_acceptable_value = 1300; img(img>max_acceptable_value) = max_acceptable_value;     % Plot the images f1 = figure(); tgroup1 = uitabgroup('Parent',f1); tab(1) = uitab('Parent', tgroup1, 'Title', 'Raw image'); ax(1) = axes('parent',tab(1)); imagesc(img) axis equal axis([0,size(img,2),0,size(img,1)]+0.5) colormap(gray(256)); xlabel('x [px]') ylabel('y [px]')…

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 created an orbit of the ISS in MATLAB. I want to validate my data. How and where can I get actual data of the ISS orbit? I would need the time history of the position vectors?

5. When two frames have the same orientation, then the (W,P,R) values of their corresponding frame transformations are (a) zero (b) non-zero 6. The robot programmer sets up UT[1] for a sharp-tip pointer that is held by the robot gripper. If UT[1] is accurate, it means that (a) UT[1] is activated in the robot system (b) The origin of UT[1] frame in the robot system is exactly at the tip of the actual pointer (c) The origin of UT[1] is aligned with the origin of Def-TCP frame

I am trying to plot an orbit in MATLAB. There is something wrong with my code because the final values I get are incorrect. The code is shown below. The correct values are in the image.     mu = 3.986*10^5; % Earth's gravitational parameter [km^3/s^2] % Transforming orbital elements to cartesian coordinate system for LEOa_1 = 6782.99;e_1 = 0.000685539;inc_1 = 51.64;v_1 = 5;argp_1 = 30;raan_1 = 10; [x_1, y_1, z_1, vx_1, vy_1, vz_1] = kep2cart(a_1, e_1, inc_1, raan_1, ...                                            argp_1, v_1); Y_1 = [x_1, y_1, z_1, vx_1, vy_1, vz_1];   % time_span for two revolutions (depends on the orbit)t1 = [0 (180*60)];  % Setting tolerancesoptions = odeset('RelTol',1e-12,'AbsTol',1e-12); % Using ODE45 to numerically integrate for LEO[t_1, state_1] = ode45(@OrbitProp, t1, Y_1, options);       function dYdt = OrbitProp(t, Y)     mu = 3.986*10^5; % Earth's gravitational parameter [km^3/s^2]   % State Vector x = Y(1); % [km] y = Y(2); % [km] z = Y(3); % [km] vx = Y(4);…

Please Solve correctly [ Mechanical- Dynamics]