rich_hodgetts
Jan 03, 2007, 03:21 PM
I have designed and flown a small depron flat plate model powered by an internally mounted 64mm ducted fan. In its original incarnation it had a pure delta wing section and whilst it flew well it lost a lot of speed when in a turn and during other high alpha manouvers.
I have redesigned the model with a cranked delta wing in an effort to gain some of the qualities of both delta and traditional planforms.
I am wondering however how this might affect the flight charachteristics of the model. I studied aeronautical engineering at university buy none of my old textbooks have any information on this somewhat unusual planform. I believe that is suffers from a pitch up problem as the angle of attack increases due to the sudden increase in vortex stregth from the highly swept inboard section. I was also wondering how far back the centre of pressure can be expected to be compared to its pure delta cousin.
Any info from those in the know would be appreciated. As its a simple model I ought to just make it and try it but I kind of want to understand the aerodynamics first!
Thanks
Rich
I have redesigned the model with a cranked delta wing in an effort to gain some of the qualities of both delta and traditional planforms.
I am wondering however how this might affect the flight charachteristics of the model. I studied aeronautical engineering at university buy none of my old textbooks have any information on this somewhat unusual planform. I believe that is suffers from a pitch up problem as the angle of attack increases due to the sudden increase in vortex stregth from the highly swept inboard section. I was also wondering how far back the centre of pressure can be expected to be compared to its pure delta cousin.
Any info from those in the know would be appreciated. As its a simple model I ought to just make it and try it but I kind of want to understand the aerodynamics first!
Thanks
Rich