A Matlab introductory class Problem.
The book for my class is "Introduction to MATLAB For Engineers, Third edition by William J. Palm
I have solved the top speed, the time to reach top speed, and the speed the plane takes off at.
this is what I have.
I need help on the graphing portion of the problem
I will give you a Thumbs Up if you solve this part for me. Thank
You.
A Matlab introductory class Problem. The book for my class is "Introduction to MATLAB For Engineers,...
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Consider the aircraft model shown in Figure 1. We will assume that the aircraft is in steady-cruise at constant altitude and velocity; thus, the thrust, drag, weight and lift forces balance each other in the x- and y directions. We will also assume that a change in pitch angle will not change the speed of the aircraft under any circumstance (unrealistic but simplifies the problem a bit). Under these assumptions the longitudinal equations of motion for the aircraft can be...
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* This is all the information given QUESTION 1 (iii,iv) PLEASE!!!: Examine the car performance when the angle of both the front and rear wings is set to θ = 10◦. In all the analysis that follows ignore frictional losses other than drag. Determine: (iii) What is the maximum speed the vehicle can safely corner a bend with R = 30 m (ans. 108Km/hr). What is the power required at this speed? (ans. 27.8KW) (iv) What is the maximum speed...
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Could i get help writing the code for this question in matlab? An internal combustion engine slider-crank mechanism is shown in the figure. Crank AB rotates in selected clockwise positive direction as shown. Piston position is Y=AD. o(t) is angular position of the crank, 0(t) is angular velocity of the crank, ő is angular acceleration of the crank. Crank AB rotates with a constant angular velocity of 5 rad/s clockwise in positive O direction as shown. Perform computer simulations using...