# Why/how is a downplane parachute configuration aerodynamically stable?

One of the most dangerous situations possible in skydiving is a so-called downplane, where both the main and reserve chutes deploy, and they shift outwards to the sides of the parachutist until essentially side-on, like so:

(Image by the United States Navy, via Wikimedia Commons; this is actually a simulation of a downplane, with two parachutists and only one parachute per parachutist, rather than the real deal, which would involve both parachutes deploying from a single parachutist, but it illustrates the configuration very nicely.)

This reduces the total cross-sectional area (as seen by the airflow) of the parachutist-parachutes assembly, causing said assembly to accelerate downwards to greater-than-optimal speeds, which is why a downplane situation is dangerous.

However, it is far from obvious how a downplane would be aerodynamically stable; even when virtually edge-on, each of the open parachutes still has a very high drag coefficient,1 a fairly low mass, and (as a result) a very low ballistic coefficient,2 while the skydiver attached to the parachutes has a fairly low drag coefficient, a much higher mass (relative to their parachutes), and, consequently, a very high ballistic coefficient. As such, the parachutist should tend to trail ahead of the two parachutes, with the aerodynamic forces on the latter wrenching them up towards top dead3 center, unless the whole shebang is spinning rapidly enough about its vertical axis for the outwards centrifugal force on the parachute canopies to overcome the upwards drag force on said canopies, which would require a spin rate high enough to be lethal even without taking parachute malfunctions into account.

What is it that overcomes these aerodynamic forces on the parachutes and renders a downplane aerodynamically stable?

1: Albeit much lower than when face-on.

2: A measure of the relative unaffectedness by aerodynamic drag of an object moving through an atmosphere of given composition.

3: No pun intended.

It appears that each parachute will tend to adopt a position where a line drawn from the skydiver through the center of pressure of the chute is aft of a line drawn through the skydiver perpendicular to the relative wind, by an angle equal to the L/D ratio of the parachute. The higher the L/D ratio of the parachute, the closer to "straight overhead" the chute can be, in the reference frame of the falling skydiver with his body positioned horizontally as per the photo. Much as the higher the L/D ratio of a kite on a string, the closer its steady-state position can approach a position straight "overhead" the kite flyer. But a stable downplane should be possible even with chutes with a rather poor L/D ratio-- the chutes just wouldn't be positioned nearly opposite each other as is the case in the photo. This would be analogous to a kite with a poor L/D ratio flying in a position that is far from "overhead" the kite flyer. The speed of such a downplane would tend to be lower than the downplane illustrated in the photo.

• (A diagram would help. PS this answer was apparently being typed and posted simultaneous w/ the other recent answer-- ) – quiet flyer Jun 22 '19 at 21:17

The parachutes are both being pulled straight down from a single point. That means the relative airflow, or angle of attack, is straight up. Lift is perpendicular to the AOA. Even if the parachutes are stalled at near 90 deg AOA at the beginning, there is still a bit of lift being produced, which acts at 90 degrees to the AOA, creating a net thrust component that causes the canopies to move away from each other, reducing AOA as they arc down, and as they become more unstalled by the reducing AOA, the lift force with net thrust component perpendicular to the AOA gets stronger, driving them away from each other harder and they arc down some more.

Eventually, as they move down to the sides, AOA continues decreasing and therefore the net thrust component of the lift force decreases, until it's small enough to be balanced by the drag of the canopies.

If the canopies move back up, AOA goes up, lift goes up, and the net thrust component goes up, driving them back down on their arc. If they move farther down, the net thrust of the lift component declines enough that drag overcomes it and moves the canopies back up. Somewhere in there, everything balances out. You are in a stable equilibrium condition.

The parachutes are in a high lift position, pulling opposite each other and so holding the parachutist up. If the parachutist drops lower, he pulls the parachutes into a higher AOA, which gives more lift, and it pulls the parachutist back up. Thus, it is stable.

• If the parachutes are pulled to a higher, liftier angle of attack, shouldn't that result in them (the parachutes) being pulled even more strongly towards top dead center, and moving even further above the parachutist? – Vikki - formerly Sean Jun 22 '19 at 21:11
• @Sean For an aircraft (such as a skydiver) which is moving straight down through the air, lift is the horizontal aerodynamic force and drag is the vertical aerodynamic force. (This is by the definitions of the words "lift" and "drag"). So, in this case, lift means the two parachutes are pulling directly away from each other. – Terran Swett Jun 23 '19 at 20:00