Welcome to the website of ME 274 for the Fall 2008 semester. On this site you can view blog posts, add your own blog posts and add comments to existing posts. In addition to the blog are links to course material: course information, information on solution videos, exams, quizzes, homeworks and other course-related material. Direct links to the homework solution videos are also available on the left side of this page.


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Jan 11, 2008

Homework Hint: Problem 2/239

Note that the "Given" information on the motion of the rocket is in terms of Cartesian components:  v = vj and a = aj. Note that v is unknown and a is known.

The "Find" information of the motion is in terms of polar components. Your task is to transform one set of components to the other set. There are a number of ways to do this. One way is to project the velocity and acceleration vectors onto the e_r and e_theta directions and solve:
  • Write e_r and e_theta in terms of i and j:  e_r = cos(theta) i + sin(theta) j and e_theta = -sin(theta) i + cos(theta) j
  • Project v onto e_r (using ve_r). Here "•" is the dot product, not a multiplication.
  • Project v onto e_theta (using ve_theta).
  • Solve the above two equations for v and r_dot using the known value for theta_dot.
  • Project a onto e_r and solve for r_dot_dot.
  • Project a onto e_theta and solve for theta_dot_dot.
Another way would be to write j in terms of e_r and e_theta. Substitute j into the above given expressions for v and a. Set these expressions equal to the polar expressions for v and a. Balance coefficients and solve. 

And there are other ways... Choose the method that works best for you.

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