What do you mean by "the load"? Anything carrying the wing is carrying the load from the wing - gravity & aero.Raptor22 wrote: It is entirely feasible that the panel carriees the front wing while the crash structure carries the load
What do you mean by "the load"? Anything carrying the wing is carrying the load from the wing - gravity & aero.Raptor22 wrote: It is entirely feasible that the panel carriees the front wing while the crash structure carries the load
Craig Scarborough @ScarbsF1
Although bonded to the nose as one piece, this is effectively what the MP4-28 modesty panel and stepped nose look like
I understood that the 'modesty panel had to be a removable panel, so how can it be bonded to the nose? If it can be bonded to the nose, then surely that makes any reference to a modesty panel. superfluous?stefan_ wrote:Craig Scarborough @ScarbsF1
Although bonded to the nose as one piece, this is effectively what the MP4-28 modesty panel and stepped nose look like
Weren't the FIA supposed to provide guidelines for what it is?gilgen wrote:I understood that the 'modesty panel had to be a removable panel, so how can it be bonded to the nose? If it can be bonded to the nose, then surely that makes any reference to a modesty panel. superfluous?
Was it supposed to be "removable" or "non-structural" (as in not a part of the main nosecone structure itself)? Or both?gilgen wrote:I understood that the 'modesty panel had to be a removable panel, so how can it be bonded to the nose? If it can be bonded to the nose, then surely that makes any reference to a modesty panel. superfluous?
I cannot locate the 'Appendix' they are referring to.(Regarding stepped noses)
3.7 Front bodywork:
3.7.9 With the exception of an optional, single piece, non-structural fairing of prescribed laminate (whose precise lay-up may be found in the Appendix to the regulations) which may not be more than 625mm above the reference plane at any point, no bodywork situated more than 1950mm forward of rear face of the cockpit entry template may be more than 550mm above the reference plane.
The external surface of any longitudinal or lateral cross section taken through the above fairing may contain no concave radius of curvature less than 50mm.
richard_leeds wrote:What do you mean by "the load"? Anything carrying the wing is carrying the load from the wing - gravity & aero.Raptor22 wrote: It is entirely feasible that the panel carriees the front wing while the crash structure carries the load
Yep. Looked there. Happy if someone else could verify. There is the 2013 & 2014 PDFs there.raymondu999 wrote:You need to download the true regulations off the FIA website. The regs PDF has all the appendices and full regs
Nope, hinge has to be at the top.allstaruk08 wrote:could they not hinge the long chord wing lower down like half way into the wing instead of at the back so when the DRS is activated it can still be aero neutral with the limited travel??