mark if 35% aft from leading edge (at mean average chord point?) is too far aft, what is the commonly accepted safe limit and where in your experience does she fly best?
> To: krnet at list.krnet.org > Date: Sun, 3 Apr 2016 19:28:49 -0700 > Subject: Re: KR> weight and balance > From: krnet at list.krnet.org > CC: ML at N56ML.com > > > Gary wrote: > > > From my plans, the CG is 15% to 40% of the wing chord. That was the old > > wing. Is it the same with to AS5048 wing? > > I don't ever remember seeing that number before. Is that for a KR1, or just > an early set of plans? My plans also say 15%-35%, and that's the range that > extends too far aft to be safe (according to an analysis by Richard Mole and > also experience by pilots). The AS50xx series airfoils are designed to have > a similar lift coefficient and range (15%-35%) as the RAF 48 (minus those > aft two inches). > > Mark Langford > ML at N56ML.com > http://www.n56ml.com > > > _______________________________________________ > Search the KRnet Archives at http://tugantek.com/archmailv2-kr/search. > To UNsubscribe from KRnet, send a message to KRnet-leave at list.krnet.org > please see other KRnet info at http://www.krnet.org/info.html > see http://list.krnet.org/mailman/listinfo/krnet_list.krnet.org to change > options
