In this project will be designed, built and tested a model of a hypothetical two-seater light aircraft with the system of connected wings.
The aim of the study is to evaluate the suitability of connected wings for a new generation of light aircraft and to collect data and experience useful for the design of such aircraft.
Model will have a wingspan of about 3 m and a weight of about 25kg . During the project numerical analyzes and measurements in wind tunnels will be carried out. The culmination of the project will be test flight.
The project is implemented by a consortium composed of:
- Institute of Aviation – leader
- Air Force Institute of Technology
- Ministry of Treasury
- Warsaw University of Technology
