deltaconfiguratie
Deltaconfiguratie, also known as a delta configuration, is a type of aircraft design where the wings are arranged in a triangular shape, with the main landing gear positioned underneath the wing. This configuration is characterized by its three main structural elements: the forward fuselage, the rear fuselage, and the central wing. The delta configuration is known for its distinctive appearance and unique aerodynamic properties.
The delta configuration was first introduced in the 1950s and has since been used in various aircraft
The delta configuration offers several advantages, including a low drag coefficient and a high lift-to-drag ratio,