Tommy Cookers wrote:n_anirudh wrote:a) There will be higher blockage and this will affect Cd Cl values
the F1 Jaguar stalled its rear wing on track at an AoA that the wind tunnel said was just fine (ask Eddie Irvine)
this was because the tunnel was too small for the model, ie just too small
naval aircraft operate unusually close to the stall in carrier approaches
public domain sources could show which ones have had problems consistent with deficiencies in tunnel size and Re number
the wind tunnel is a design tool whose cost, value and availability attributes may be competing with those of other design tools
Did CFD say the wing would not stall as well?
I guess it did as CFD usually precedes wind tunnel testing.
How close walls have to be to affect model aerodynamics?
Do circuit walls and tire barriers affect aero as well? I guess they do so the question is what is the distance threshold. Specially interesting in Monaco.
gixxer_drew wrote:With a static floor and boundary suction, everything is a generalization anyway. You can still go faster from what you learn. What level are you developing at?
You designing front diffusers or cooling systems? Big difference in what you need to go faster at the end of the day. Taking an axe to your aero or a scalpel?
Did you mean with a static floor and WITHOUT boundary layer suction?
So it looks like boundary layer suction is also good for the wind tunnel walls and ceiling, not only for the floor?