On Tue, 19 Dec 2006, Maik Justus wrote: > One important point for the simulation: most rotors have a delta3 effect > (this means: reducing the pitch with increased flapping angle). Do you > know this parameter for the ch53e (or for other helicopter?)
I can only add that the CH-47D has no delta3 mechanism. (Or at least not the RAF HC Mk2 version which is very similar to the D version Chinook. Found that out just now from reading the RAF Mull-of-Kintyre accident report more thoroughly. But presumably this goes for all Chinook production models.) ------------------------------------------------------------------------- Take Surveys. Earn Cash. Influence the Future of IT Join SourceForge.net's Techsay panel and you'll get the chance to share your opinions on IT & business topics through brief surveys - and earn cash http://www.techsay.com/default.php?page=join.php&p=sourceforge&CID=DEVDEV _______________________________________________ Flightgear-devel mailing list Flightgear-devel@lists.sourceforge.net https://lists.sourceforge.net/lists/listinfo/flightgear-devel
