Drag and Air Resistance in Ballistics

The Force That Slows a Projectile

Drag is the aerodynamic force that resists a projectile's motion through the air, acting directly opposite the direction of travel. It is the primary reason velocity decreases with distance, and understanding what drives it explains nearly every downrange effect an analyst reads in a trajectory table.

What Determines Drag

Drag depends on air density, the projectile's speed, its frontal area, and its shape. The force rises with the square of velocity, so a projectile moving twice as fast experiences roughly four times the drag force at that instant. This is why a fast projectile sheds velocity most rapidly right after leaving the muzzle, then decelerates more gently as it slows.

The Drag Coefficient and Mach Number

Aerodynamicists express shape efficiency as a drag coefficient, but that coefficient is not fixed; it changes with the ratio of the projectile's speed to the speed of sound, called the Mach number. Drag rises steeply as a projectile approaches and crosses the speed of sound, which is why the region near Mach 1 is treated as a special, less predictable regime.

Pressure Drag and the Boat-Tail

Much of a supersonic projectile's drag comes from the pressure difference between its nose and its base, including the low-pressure wake behind a flat base. Tapering the rear into a boat-tail shrinks that wake and reduces base drag, which is a major reason modern long-range designs use boat-tail geometry rather than flat bases.

Air Density and Environment

Because drag is proportional to air density, environmental conditions matter. Thinner air at high altitude or high temperature produces less drag, letting a projectile fly flatter and retain velocity longer, while cold, dense, sea-level air does the opposite. Ballistic solvers require these atmospheric inputs for this reason.

Worked Example

Suppose a projectile leaves the muzzle at 3,000 feet per second and loses about 300 feet per second in its first 200 yards. Over the next 200 yards it might lose only around 250 feet per second, and less still in the interval after that. The deceleration eases as the projectile slows because drag force scales with the square of speed, so the biggest velocity losses always occur early.

A Common Misconception

Many readers assume drag slows a projectile at a steady, constant rate over its flight. It does not. Drag force depends on the square of velocity, so deceleration is greatest near the muzzle and diminishes as the projectile slows. This changing rate, not a fixed one, is why velocity-loss curves bend rather than fall in a straight line.

Explore the glossary.

Source: National Institute of Standards and Technology (NIST) Fluid Dynamics Reference — Federal Metrology Standards Reference. Refer to the original for exact language.