wing loading

Wing loading has an effect on an aircraft's climb rate.

Landing is also a problem for large birds with high wing loadings.

They were also concerned about the high wing loading.

All the early aircraft had very low wing loadings for sufficient reasons.

Their small wings give them a high wing loading.

It has a low wing-aspect ratio and high wing loading.

The wing loading must be very low in order to allow the pilot to run fast enough to get above stall speed.

The smaller the wing loading, the tighter the turn.

They are heavy for their size with a high wing loading, so they need to fly fast.

Wing loading is the ratio of weight to wing area.

Mass-carrying ability, for example, is most closely linked with wing loading.

Therefore, flight speed is proportional to the square root of wing loading.

These recovered some of the field performance lost as a result of the Galaxy's higher wing loading.

To reduce wing loading, load alleviation systems were added to the aircraft.

It was also specified that the wing loading should be kept below 100 kg/m.

Estimates of its body weight and wing loading suggest that it was largely ground-dwelling.

The plane had good handling, except for take-off and landing, which were difficult due to high wing loading.

The wing loading is important in determining how rapidly the climb is established.

Most student skydivers fly with wing loadings below one pound per square foot.

Wing loading is a useful measure of the general manoeuvring performance of an aircraft.

The relatively high design wing loading of 7 pounds per square foot might increase speed, but decrease manoeuvrability.

The F-16 has a moderate wing loading, which is lower when fuselage lift is considered.

These measurements show that M. lyra have a low wing loading and aspect ratio.

Its size and weight meant that it had high wing loading, which limited its maneuverability.

Professional Canopy pilots compete at wing loadings of 2 to 3+ pounds per square foot.