1.

 
100% of survey complete.
Please think how you learned this section. What did you find to be helpful? Please tick all that apply.

Question Title

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

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

Question Title

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

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

Question Title

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

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?

Question Title

* 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?

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?

Question Title

* 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?

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?

Question Title

* 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?

What are the boundary conditions used with the linearized potential equation?

Question Title

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

What is the planar wing approximation?

Question Title

* 8. What is the planar wing approximation?

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

Question Title

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

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

Question Title

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

T