Firstly i would like to thank for al those kind souls out there whom have taken the time to view my post.
I have attached a diagram to this post. Hopefully it helps you visualise my quries. The diagram is not to scale, neither it is the actual aircraft design.
If you do not understand specific parts of my question, Please kindly inform me and feel free to correct me if im wrong. Thankyou again for your time and expertise.
Im embarking on a new project which has a very high importance to me and my grades at school. Im starting a year earlier for the project so that i can get things going at prototype stage.
Current Technical Details
Aircraft Type : VTOL/STOL
Aircraft Propulsion: Ducted Fan, Electric Motors
Aircraft Approx Length ( From Nose to Tail): +1.4 Metres (4.59 feet)
Aircraft Payload Capability : FPV Devices
Control Surfaces : Elevator, Rudder, Ailerons , Flaps
Budget Cost: To Be Confirmed
Type of Technology to Incoporate : Vectored Thrusting 0-90 Degrees Tail Movement, Downwards Thrust
Landing Gears: Yes
Aircraft Structure : Composite Shell Structure( Secondary) with Internal Structure( Primary) mounts.
Other Comments : Rear Propulsion fan will divert thrust downwards and eventually convert to vertical thrusting,and back up to horizontal as well.During VTOL, The three mid fans on the fueslage and wings along the CG line willbe thrusting downwards to ensure even distribution of weight, Most of the batteries, stuff will be located on the horizontal CG line from the top.
Current Questions Regarding the Project for now.
1. Do you think such a configuration would work?
2. What are your views and reccomendations that i can consider.
3. If so what kind of setup would be best regarding the following
[*]Type of connections to take note[*]Reccomended Ducted Propulsion Size[*]Type of Electronic Arrangement to take note E.g ESC connected to the Motors[/list]