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Lutz Möller
Lutz Möller
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Didion

Wind drift Approximation derivation

Lateral Crosswind Bullet deflection

Alan D. Peake April 2000

The following assumptions are made:

  1. The Drag coefficient is for all Bullet velocities constant.

  2. The Bullet yaws not.

  3. The Bullet velocity is always much greater than any Wind speed.

Drag Coefficient Projectile Mass Air Density Projectile Reference Area
= Bullet Velocity

= Bullet Acceleration
Muzzle velocity lateral Bullet velocity forward Bullet velocity
vx lateral Bullet velocity ax lateral Bullet acceleration forward Bullet acceleration
lateral Wind forward Wind

is the Projectile Forward velocity (Ballistic wind) and Crosswind combined Airflow.
is the total Projectile drag force.
Since F = m · a, the Bullet accelerates
Let , so that simplified , or
Now assume and , then
When is the Lateral wind to Bullet forward velocity Angle, then

As and the lateral acceleration is or (1)
Similarly for small the forward acceleration is The Minus sign means, the Bullet slows.
The Velocity time differential is Acceleration. So integrating yields the Velocity.
So integrated gives
At , so the forward velocity becomes (2)
Similarly, to find the lateral velocity, we integrate the lateral acceleration from (1)
so substituting

for (1) we get Rearranging the terms yields
Integrate both Sides to
At , so giving or
By rearranging, the lateral velocity is (3)


We now need the Time for the Bullet to reach the Downrange distance
and so from (2) integrated gives
At , so thus and therefore (4)
Substituting (4) in (3) for leads to and integrating gives (5)
So from (4), or
then (6)
Remembering for the lateral Movement or Deflection we thus have an expression in Drag coefficient terms.

While equation (6) is not intuitive, it clearly shows the Deflection behaves to Muzzle velocity inversely proportional.

To rewrite (6) as

and substitute (4) leads to the Didion Equation
The term is the Difference between Flight time in Vacuum and actual Flight time, or the "Lag" time.

Hence is Didion's Approximation called the "Delay Lag Theory". Given only the Drag coefficient and bullet dimensions, Deflection cannot directly be calculated. However, if the actual Flight time can be measured or calculated, then to calculate the Wind deflection is quite simple.

Mr. Moeller,

Wonderful! Thank you for publishing the Didion Approximation for Wind drift article! as a novice target shooting enthusiast, I've long suspected the existence of the conditions described in the paper, but never had a good mathematical handle on them. I very much appreciate seeing the sound and straight forward treatment of wind drift modeling given in the approximation. Thank you again!

FYI: I first downloaded the .doc version which contains a small error as follows: the second equation describes the total drag force on the projectile, which is then divided by the mass of the projectile to obtain the third equation describing the acceleration (deceleration) of the projectile. In that expression for acceleration, the coefficient of drag is missing. The same error appears in the HTML version of the same article. As a minor comment, English readers are accustomed to seeing the character "e", as is used in the article, rather than the Greek character epsilon, to represent the natural base. Anyone with a mathematical background will certainly understand the article, however, and epsilon vs. "e" is not a flaw.

Best regards,

Bob Porter, Sonntag, 13. April 2003 07:00

Lutz Möller