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Drag Coefficient |
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Projectile Mass |
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Air Density |
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Projectile Reference Area |
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= Bullet Velocity |
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= Bullet Acceleration |
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Muzzle velocity |
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lateral Bullet velocity |
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forward Bullet velocity |
vx |
lateral Bullet velocity |
ax |
lateral Bullet acceleration |
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forward Bullet acceleration |
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lateral Wind |
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forward Wind |
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is the Projectile Forward velocity (Ballistic wind) and Crosswind combined Airflow. |
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is the total Projectile drag force. |
Since F = m · a, the Bullet accelerates |
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Let |
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, so that simplified |
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, or |
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When |
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is the Lateral wind to Bullet forward velocity Angle, |
then |
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As |
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and |
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the lateral acceleration is |
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or |
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(1) |
Similarly for small |
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the forward acceleration is |
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The Minus sign means, the Bullet slows. |
The Velocity time differential is Acceleration. So integrating |
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yields the Velocity. |
So |
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integrated gives |
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At |
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, |
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so |
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the forward velocity becomes |
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(2) |
Similarly, to find the lateral velocity, we integrate the lateral acceleration |
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from (1) |
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so substituting |
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for (1) we get |
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Rearranging the terms yields |
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Integrate both Sides to |
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By rearranging, the lateral velocity is |
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(3) |
We now need the Time for the Bullet to reach the Downrange distance |
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and so from (2) |
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integrated gives |
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At |
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, so |
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thus |
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and |
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therefore |
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(4) |
Substituting (4) in (3) for |
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leads to |
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and integrating gives |
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(5) |
So from (4), |
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or |
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then |
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(6) |
Remembering |
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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 |
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and substitute (4) leads to the Didion Equation |
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The term |
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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.php 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