KR>Forward c of g
My Taylor Mono Plane (almost identical to the KR1 except my horizontal stab is larger) has a forward c of g condition depending on fuel loading ( I have a rear fuel tank as well as forward. Can any one tell me with experience how much of a forward c of g they have flown and how did it perform? I'm looking at a 18.2% MAC full fuel in forward tank with zero in aft tank. My target is 11.40-15.90 of the RAF48" cord Or 23.75 to 33.125% of MAC If I can provide flying surface dimensions could some one run them on one of the good airplane design soft ware packages for me? Darren Pond Taylor Mono Plane CF-VML KR2 C-GGGW
KR>Forward c of g
Darren and others, Chris Heintz in his Heintz' Textbook series provides all the info you need to calculate the c of g range of your aircraft. You will find it at: http:/www.zenithair.com/kit-data/ht-90-4.html Gene Lukan - Original Message - From: "Darren Pond" <pon...@rogers.com> To: "KR builders and pilots" <kr...@mylist.net> Sent: Saturday, May 31, 2003 12:08 PM Subject: KR>Forward c of g http://www.krnet.org/instructions.html
KR>Forward C of G on KR1
> > > HI all > Just finished my Weight and balance on the Taylor Mono plane (grandfather > of the KR) My worst case forward C of G has me at the 18% of MAC. Any one > with experience with flying forward C of G? > > Darren Pond -- next part -- A non-text attachment was scrubbed... Name: winmail.dat Type: application/ms-tnef Size: 1704 bytes Desc: not available Url : http://mylist.net/private/krnet/attachments/20030526/03986ad8/winmail.bin
