Since a sailplane is focused on performance - what with tricky laminar flow airfoils and all.

Eo why this

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Instead of this

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It looks to me like that long tail is needed to balance the cockpit. Buy then why not just put the wings beside the cockpit?

Even if we cannot use a flying wing, why not s least a shortened tail? Why this weight and drag penalty?

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    $\begingroup$ Here is an example of an actual shortened tail glider : Genesis II $\endgroup$
    – jkztd
    Feb 23, 2021 at 12:16
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    $\begingroup$ The Genesis isn't really a "shortened tail" regular glider. It's a flying wing glider, designed by Jim Marske, who wanted to keep it a pure flying wing, but was browbeaten by his financial backers into putting a little horizontal trimming surface at the top of the fin. They eventually threatened to pull their backing if it didn't have a surface there, as they thought it would limit sales without it. Its horizontal "tail" is a redundant appendage stuck there to keep his partners happy. $\endgroup$
    – John K
    Feb 23, 2021 at 14:09
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    $\begingroup$ @JohnK yet it is at least an all-moving trimmer. I thought about this because it's the closest match to OP shortened tail concern. Indeed looking at the small horizontal stabilizer volume, wing's airfoil has to be reflex. $\endgroup$
    – jkztd
    Feb 23, 2021 at 14:25
  • $\begingroup$ @qqjkztd that thing is a flying outrage! Also, I would think it needs a wash-in $\endgroup$
    – Abdullah
    Feb 23, 2021 at 15:14
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    $\begingroup$ @Abdullah Marke's designs, incl the Pioneers and the Monarch, have very nice flying qualities as flying wings go. The forward sweep is modest and is offset by generous fin area and give decent yaw stability by glider standards. They are effectively spin proof because the forward sweep inhibits tip stall and the inboard wing, where the elevator is, cannot be brought to stalling AOA because the elevator unloads as soon as the flow at the TE starts to separate. As a result, you don't need wash-in, which promotes tip stalls and spins. $\endgroup$
    – John K
    Feb 23, 2021 at 15:28

2 Answers 2


Keep in mind that not all sailplanes are designed for extremely light weight. Decreasing the weight also decreases the minimum sink rate, but doesn't help the still-air glide ratio, and actually hurts the glide ratio against a headwind.

Even in sailplanes that are designed for very light weight, designers have sometimes thought it worthwhile to employ a rather large vertical fin. A good example of this is the Carbon Dragon.

The basic purpose of a vertical fin is to prevent the aircraft from flying sideways through the air, especially when the pilot makes an aileron input, which tends to create adverse yaw. Adverse yaw tends to be most pronounced in long-spanned, slow-flying aircraft.

Flying sideways is never efficient.

However, not all sailplane designers have always followed this philosophy. The Scheibe Bergfalke is an example of a glider with a rather small vertical fin. (Look closely at photos of this glider and you'll see that more than 75% of what appears to be the "tail" is actually the rudder, not a fixed vertical fin.) When flown with the pilot's feet off the rudder pedals, it tends to be rather uncooperative in response to aileron inputs, being quite happy to fly sideways through the air rather than actually turning.

Keep in mind also that a given desired "tail volume"-- the product of tail area times moment-arm-- can be achieved with less drag with smaller tail on a long slender boom (rear fuselage), than with a larger tail on a shorter fuselage. You've really asked two separate questions here-- "Why is the tail boom so long?", and "Why is the vertical fin so large?". The first question is easier to answer than the second-- the tail boom itself creates relatively little drag, due to its slender cross-section and resulting low "wetted area". To a first approximation, we can say that the tail boom is long so that the fin and horizontal tail don't need to be larger, to create the desired tail volume and flight characteristics. In truth, the story is a little more complicated-- when we dive into the details of spiral stability theory, we find that extending the tail boom while keeping the "tail volume" the same actually does produce significant changes in the aircraft's flight characteristics, due to that fact that the airflow and "relative wind" are actually curved whenever the flight path is curved.1 This also means that for a given "tail volume", the drag reduction resulting from extending the tail boom and decreasing the tail area will be less in turning flight than in linear flight.

One reason that modern sailplanes are generally designed with much larger vertical tails than vintage sailplanes--or most single-engine general aviation aircraft-- is that the long slender tail booms used in modern sailplane designs have a very small cross-sectional area and thus contribute very little to the aircraft's yaw stability ("directional stability"). Nearly all of the required "weathervane effect" has to come from the tail itself.

Certainly the purpose of the long tail boom and large vertical fin is not to "balance" the weight of the cockpit. Rather, the cockpit is placed in the optimum position to balance everything else.


  1. Re "the airflow and 'relative wind' are actually curved whenever the flight path is curved"-- another way to say this is to note that in curving flight, the aircraft is rotating as well as translating linearly, so at any given instant in time, different parts of the aircraft are moving through the airmass in different directions. The instantaneous linear velocity at the nose and tail are different, and "tufts" or "telltales" at the nose and tail would not blow in the same direction. Details of the effects of the curving relative wind are beyond the scope of this answer, but it may be interesting to compare and contrast the designs of competition-level radio-controlled model sailplanes versus "free-flight" model sailplanes. Both have relatively long fuselages, but the former invariably have much larger vertical tails than the latter. The latter must be designed to fly in stable circles with no pilot input, while the former are designed for good response to pilot control inputs. The effects of the curving airflow in turning flight play a role in these dynamics.
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    $\begingroup$ Isn't there also a speed factor involved? That is, the force on the tail is proportional to the airspeed, so a plane designed to fly slowly would need a larger tail to supply a given force, $\endgroup$
    – jamesqf
    Feb 23, 2021 at 16:42
  • $\begingroup$ One more tidbit of info: I was told that sailplanes have T-tails in order to be able to survive landing in fields with high grass or eg wheat. $\endgroup$
    – ghellquist
    Feb 23, 2021 at 17:03

Gliders spend a lot of time circling, entering thermals dodging others while ridge flying and generally performing manoeuvres designed to terrify most power pilots. Henry Ford remarked 'there is no substitute for litres'. For a glider pilot 'there is no substitute for span'. Mine is a titchy 15 meters. And even that represents a very large moment of inertia in the yaw axis. To enter circle you have to simultaneously increase the rate of yaw and pitch. Back on the pole then and a boot on the rudder (hopefully coordinated otherwise we go skidding all over the sky!). You can only get the moments needed from elevator (pitch) and rudder (yaw). The wing tips might offer a longer arm but there are issues with sticking control surfaces there. (Spin, anyone?)


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