Topic 4 - External Ballistics Flashcards
What dictates the path of a projectile?
- Gravity
- Angle of launch
- Velocity
- Air density, temperature & humidity
- Projectile shape (drag coefficient & projectile stability)
What SUVAT equation would you use for a horizontal launch (zero-degree elevation so the trajectory starts at its maximum height) for the y-direction?
S = ut + 1/2at^2
u = 0 so s = 1/2 at^2
What equation could you use in the x-direction when there is no air resistance and no deceleration?
Ux = Sx / Ttotal
What suvat equation can be used if the launch and impact sites are on the same horizontal plane?
S = (u^2sin(2angle) / g
What is aerodynamic drag typically proportional to?
Aerodynamic drag is typically proportional to the square of the velocity, so drag builds significantly with velocity.
What factors contribute to drag?
- The profile or shape of the projectile.
- The cross-sectional area of the projectile in the direction of travel.
- Air density.
What is the centre of mass (also known as the center of gravity / CoM / CoG)?
The point where the bullet balances its weight
Like the pivot point on a see-saw
What follows the trajectory when in flight?
The center of mass is the only point of the bullet that follows the trajectory when in flight.
What is the center of pressure (CoP)?
The center of pressure is the point where the aerodynamic forces act after adding up all of them.
In the case of a bullet, it will be the sum of the drag forces from the air flow.
How is drag stabilisation acieved?
- By adding fins which creates additional drag forces at the rear of the projectile.
- This brings the CoP rearward of the CoM leading to a smaller and less influential turning moment.
- This results in a stable flight path without the need for and gyroscopic stabilisation
How can the total drag force experienced by a projectile be calculated?
Fd = 1/2CdAV^2p
Fs = Drag force in n
Cd = Drag coefficient
V = flow velocity in m/s
A = cross-sectional area
p = air density @ sea level (about 1.2 kg/m^3)
What can wind tunnels be used to measure?
Wind tunnels can be used to measure the drag force experienced by a projectile design as air is blown over a stationary object.
How do you calculate drag coefficient (Cd)?
Cd = 2Fd / AV^2p
What is the Mach number?
It defines how many times the speed of sound the projectile is moving at?
How do you calculate sectional density?
S = m /d^2