The defintion of a Postive Static Stability is

What typically arise from the aircraft’s mass distribution in response to linear and angular accelerations?

When in equalibrium, to balance the forces, the accleration in the direction of the force is required

Further increasing the sweep back angle on the wings will [blank1] lateral stability and therefore a [blank2] type wing is required

When the airplane is in a bank, the aerodynamic forces tend to turn the plane more deeply into the bank, and the nose drops, resulting in an ever-tightening downward spiral with increasing airspeed

For a propeller driven aircraft, the thrust required is a function of what 2 variables?

Relative to propeller driven engines, fuel flow is a function of

The minimum point in the airspeed versus fuel fuel flow curve will correspond to the conditions for best:

The parts of the airplane that have the greatest effects on dampening are what

High wing airplanes have the benefit what structural to add laterial stability