1.

 
100% of survey complete.

* 1. Please think how you learned this section. What did you find to be helpful? Please tick all that apply.

* 2. Please list the top 5 concepts that you learned in this module.

* 3. What concepts pose(d) difficulties for you? Please discuss, and also how you solved the difficulty if you did.

* 4. Which terms that are neglected in the linearization, become large under transonic conditions? So what would be a good form of the equation valid for transonic conditions?

* 5. Which terms that are neglected in the linearization, become large under hypersonic conditions? So what would be a good form of the equation valid for hypersonic conditions?

* 6. Why is it that the linearized pressure coefficient in compressible potential flow, depends only on the fluctuation in the velocity component along the freestream direction?

* 7. What are the boundary conditions used with the linearized potential equation?

* 8. What is the planar wing approximation?

* 9. How do we use the linearized potential equation to solve for the lift and pitching moment of a wing in subsonic compressible flow?

* 10. If the objective is to match pressure distributions between two subsonic Mach numbers, what transformation would you use?

Report a problem

T