*from the link Jesse provided*
This is for F=MA ....
Just liked you explained how you came to your screen name
FORCES ON AN AIRFRAME
"The dynamic pressure on an airframe is defined as the maximum pressure force available in a flow field relative to the true airspeed. These forces are defined by the equation: q = 1/2 σ V ^2 with "σ" defined as air density on a vehicle and “V†as the velocity in ft/sec.
An example of force (pressure) acting on the forward facing surfaces of a typical model jet such as a BVM Ultra Bandit is:
25.2 lb/sq ft at 100 mph
56.7 lb/sq ft at 150 mph
100.8 lb/sq ft at 200 mph
157.5 lb/sq ft at 250 mph
226.8 lb/sq ft at 300 mph
308.8 lb/sq ft at 350 mph
The effect of speed and radius of the turn on “G†forces is:
F = (mv^2)/r where “F†is force, “r†is radius, “m†is mass and “v†is velocity
As the true airspeed of an aircraft doubles from 150 mph to 300 mph, it experiences four times the “G-loading†when performing a simple level turn of a similar radius. This means that even a large ¼ mile radius (1320 foot) turn requires a hefty 4.56g “pull†at 300 mph under standard, sea level conditions while it’s only 1.14g at 150 mph. Additionally, when this turn radius is halved to 1/8 mile, the load factor doubles to 9.12g! Thus it is easy to envision how more aggressive maneuvering required to keep a 300 mph aircraft in comfortable visual range or to set up for speed runs can easily impact huge aerodynamic loads on a structure.
Every control surface has a critical flutter speed dependant on its area, weight, hinge moment, and electro/mechanical control system."