Model of "Inovative composite ultralight two-seater plane"

  • Posted on: 3 September 2015
  • By: BB composite
MODEL OF "INOVATIVE COMPOSITE ULTRALIGHT TWO-SEATER PLANE"

Non-standard "Three lifting surface" configuration with a modified tandem wing connected to the integral structure of high bending stiffness and with fuselage designed to give a great contribution to lifting force, ensuring high aerodynamic and structural advantages over the classic conception.

As a consequence, should have the following characteristics:

Length 3.85m
Wingspan 5m
Take-off distance up to 60m
Climbing rate 12,5m/s
Expected high maximum speed Vmax 350km/h
High cruising speed   Vcr 320km/h
Range with 50 l of unleaded gasoline 1600km
Flying at extreme angles of attack up to 30
Safe flying secured from falling into STALLING  

Engine: BMW Boxer R 1.2 GS, max. power 115hp, consumption of 9l/h unleaded gasoline at cruising mode

Model of a given aircraft is made in proportion of 40% for verification the stability and controllability and lifting characteristics. Conducted tests of the model have confirmed exceptional handling and stability in a wide range of gravity position so as an excellent lifting force characteristics of applied concept. Stall occurred at a speed of 50km / h and the angle of attack of 25

Computer simulation of the airflow around the wings Computer simulation of the airflow around the wings

Computer simulation of the airflow around the canardComputer simulation of the airflow around the canard

RenderRender

RenderRender

Master modelMaster model

Final model of the planeFinal model of the plane

Final model of the planeFinal model of the plane

Final model of the plane Final model of the plane

Final model of the planeFinal model of the plane