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Aviation

Glide distance calculator

How far an aircraft glides from a given height at its best glide ratio, adjusted for a headwind or tailwind, and the height needed to reach a field.

Published 9 October 2026

What this calculator does

A glide ratio of nine to one means nine units forward for every one down, which from 5,000 feet above the ground gives 7.4 nautical miles in still air. That is the headline number, and the useful one is what the wind does to it.

Wind changes the distance without changing the descent rate at all. The aeroplane still takes six minutes and twenty-one seconds to reach the ground from 5,000 feet; it simply covers less ground doing it. A 20 knot headwind on a 70 knot glide cuts the range from 7.4 miles to 5.3 and the effective ratio from nine to 6.4.

The formula

Formulastill-air distance = height × glide ratio ÷ 6076.12; wind changes the groundspeed and so the effective ratio becomes ratio × groundspeed ÷ airspeed

Still-air distance is height × glide ratio ÷ 6076.12. The descent rate follows from the airspeed and the ratio, and the time to the ground follows from the height and that rate. Distance over the ground is then groundspeed times that time, where groundspeed is airspeed less the headwind component. The effective glide ratio is the book ratio scaled by groundspeed over airspeed.

TermMeaning
Glide ratioForward distance per unit of height lost, at the best glide speed in the configuration the manual specifies.
Best glide speedThe airspeed that achieves the book ratio. Flying faster or slower than it costs distance.
Effective ratioThe book ratio adjusted for wind. What you actually get on the day.
Height above groundNot altitude above sea level. The difference matters over terrain.

The inputs explained

FieldWhat to enter
Height above the ground (ft)Height above the ground you are gliding over, not altitude above sea level.
Best glide ratio (:1)Best glide ratio from the flight manual. Typical light singles sit between 7 and 10 to 1.
Best glide airspeed (kt)Best glide airspeed from the manual. The ratio only applies at this speed.
Headwind component (kt)Headwind component along the glide. Enter a negative figure for a tailwind.
Distance to the field (nm)Distance to the field you are considering, used for the height needed and the margin.

When to use it

Working out what is within reach

Enter your height and the distance to a candidate field. The height needed and the spare height are the two numbers that answer whether it is reachable, and the margin should be generous rather than exact.

Understanding why into-wind is expensive

A 20 knot headwind on a 70 knot glide removes nearly 30 per cent of the range, because it removes 30 per cent of the groundspeed while the aircraft sinks at the same rate. Downwind options are worth considerably more than they look.

Checking a published glide ratio

Set the wind to zero and compare the still-air distance against the rule of thumb you were taught. Many are conservative, which is the right direction, but knowing by how much is useful.

Worked examples

Every figure in the tables below is produced by this page’s own calculator at build time, so the numbers and the tool always agree. Select any row to load that scenario.

How far can you glide from each height?

Only the height above the ground changes.

9:1 glide ratio at 70 kt, still air
Height above groundGlide distanceTime to the groundHeight you have spare
1,000 ft1.48 nm1 min 16 s-2,376 ft
2,000 ft2.96 nm2 min 32 s-1,376 ft
3,000 ft4.44 nm3 min 49 s-376 ft
5,000 ft7.41 nm6 min 21 s1,624 ft
8,000 ft11.85 nm10 min 9 s4,624 ft
10,000 ft14.81 nm12 min 42 s6,624 ft
The distance is a straight line in height: 1.48 nautical miles per thousand feet at this ratio, so 1,000 feet gives 1.48 miles and 10,000 gives 14.81. The time is equally linear at 1.27 minutes per thousand feet. Reaching the five mile field in the last column needs 3,376 feet, so the 3,000 foot row is the last one that falls short, and it misses by 376 feet.

What does wind do to the glide?

The height and the aircraft are identical. Only the wind along the glide changes.

5,000 ft above ground, 9:1 at 70 kt, field 5 nm away
HeadwindGlide distanceEffective glide ratioHeight needed to reach the field
20 kt tail9.52 nm11.57:12,625 ft
10 kt tail8.46 nm10.29:12,954 ft
0 kt head7.41 nm9.00:13,376 ft
10 kt head6.35 nm7.71:13,938 ft
20 kt head5.29 nm6.43:14,726 ft
30 kt head4.23 nm5.14:15,907 ft
A 20 knot tailwind gives 9.52 miles at an effective 11.57 to 1. A 20 knot headwind gives 5.29 miles at 6.43 to 1. That is a spread of more than four miles on the same aircraft at the same height, and the height needed for the five mile field runs from 2,625 feet downwind to 4,726 upwind. The descent rate is 788 feet a minute in every row, because wind does not change how fast an aeroplane sinks.

Questions

Why does wind change the distance but not the descent rate?

Because the aircraft descends through the air at a rate set by its airspeed and configuration, and the air is moving over the ground independently. The time to the ground is unchanged; only the ground covered in that time moves.

Does a windmilling propeller matter?

A great deal. Book glide ratios usually assume the propeller in a specific condition, and a windmilling propeller on a failed engine creates substantial drag that can cut the ratio noticeably. This calculation uses whatever ratio you enter.

Should I use height above ground or altitude?

Height above the ground you intend to glide over. Using altitude above sea level over high terrain will overstate the distance by exactly the terrain elevation times the glide ratio.

Is flying faster than best glide ever better?

Into a strong headwind, slightly, because spending less time in the wind can beat the lost ratio. The effect is small and the speed increase modest, and this page does not model it, so treat the book speed as the default.

How much margin should I leave?

More than the arithmetic suggests. The figures here assume best glide speed held precisely from the moment of failure, a clean aircraft and an accurate wind, and none of those is reliable in the first thirty seconds of a real engine failure.

For the descent planning version of the same geometry, see top of descent. Wind along the glide can be resolved with wind correction angle, and fuel burn endurance and range covers the case where the engine is still running.