Ground Effect
Ground effect is the aerodynamic phenomenon that arises when an aircraft flies close to the ground — within about one wingspan in height.
Mechanism
The ground disturbs wingtip vortex formation:
- Downwash reduced: less downward-directed flow under the wing.
- Wingtip vortex weaker: vortices cannot fully develop because the ground inhibits them.
- Effective angle of attack of the wing becomes larger (less downwash).
- Induced drag drops drastically (typically 40-60 % at 0.1 spans height; Anderson Ch. 5).
- Lift coefficient rises at the same α.
Height dependence
Effect strength depending on the ratio height/wingspan:
| Height / wingspan | Induced drag reduction | Applicable |
|---|---|---|
| 1.0 | < 5 % | practically gone |
| 0.5 | 15 % | noticeable |
| 0.25 | 30 % | distinct |
| 0.1 | 50–60 % | very strong, take-off / landing |
Cessna 172 with 11 m span: ground-effect range about 0 to 11 m AGL.
On take-off — pros and cons
Pros
- Aircraft "lifts off earlier" than the performance table suggests (less induced drag → less power required).
- Soft-field take-off: after lift-off, accelerate in ground effect to Vy → only then climb.
Cons / traps
- "Aircraft lifts off, can't climb": if you "leave" in ground effect but lack speed for climb → climb attempt results in stall, because drag returns out of ground effect.
- Hot and high: ground effect can deceive — aircraft feels okay on take-off but sinks once outside ground effect.
On landing
- Flare becomes easier: lift higher, sink rate naturally diminishes → softer touchdown.
- "Floating": with too high touchdown speed the aircraft floats long — runway may be insufficient.
- Crosswind landing: ground effect can amplify drift because aircraft "floats" longer.
Pilotage recommendations
Take-off
- Performance from POH — ground effect already accounted for.
- Don't rotate too early — wait until Vr.
- Climb-out: at lift-off in ground effect, accelerate to Vx or Vy, then climb.
Landing
- Stabilised approach at Vapp.
- Over threshold: power idle, pitch up — flare begins.
- Sink rate should fall to 0 in ground effect, smooth touchdown.
- If floating: apply brakes, retract flaps (POH).
Special aspects
- WIG (Wing In Ground Effect) aircraft: specifically designed for efficient ground-effect use (e.g. ekranoplan, Caspian Sea Monster) — can only fly just above water.
- Birds use ground effect instinctively (gulls over water).
- Helicopters: similar effect in hover (IGE/OGE — In/Out of Ground Effect).
POH performance tables
Take-off distance and landing distance in POH tables are determined under standard conditions (ISA, MSL, no wind, hard runway). Ground effect is included — but actual wind, runway state, altitude, temperature must be accounted for separately.