Hi all,
I am helping someone study and was looking over some practice FAA tests. As an engineer, some of their reasons bother me. For example, they always seem to conflate the point of minimum drag with the point of max L/D. They always show the point of minimum drag on the curve, but refer to it as max L/D.
Here's another one for you... how would you answer this?
I am helping someone study and was looking over some practice FAA tests. As an engineer, some of their reasons bother me. For example, they always seem to conflate the point of minimum drag with the point of max L/D. They always show the point of minimum drag on the curve, but refer to it as max L/D.
Here's another one for you... how would you answer this?