The He 219 was particularly prone to this; its high wing loading at the edge of stalling speed left it unmanoeuvrable.
12.
All three factors increase stalling speed and reduce aircraft performance, making it very difficult to climb or even maintain level altitude.
13.
The A & AEE found that the maximum speed of the biplane configuration was slower than the stalling speed of the monoplane configuration.
14.
In the early 1930s the French Navy became interested in stalling speed of less than 100 km / h ( 62 mph ).
15.
The airspeed at which this angle is reached is the ( 1g, unaccelerated ) stalling speed of the aircraft in that particular configuration.
16.
This required an even lower stalling speed, which in turn required a low wing loading, combining both large wing area with light weight.
17.
Retractable slats, as seen on most airliners, provide reduced stalling speed for take-off and landing, but are retracted for cruising.
18.
In response to the request for proposals, the Navy received designs from Stearman Aircraft, flaps on the upper wing to reduce stalling speed.
19.
The inclusion of full span automatic leading-edge slats, The slats lowered the stalling speed of the aircraft to roughly depending on load out.
20.
This arrangement reduced stalling speed and increased lift, allowing the aircraft to use a smaller wing compactness being an important feature for a ship-borne aircraft.
