>
> --------------------------------------------------
> From: <cas...@mminternet.com>
> Sent: Thursday, March 31, 2011 4:03 PM
>>
>> please cite a source rather than a general statement.
>
> Well you could try section 4.4 of the Datcom (not digital datcom). This
> text
> is available at
> http://openae.org/stability-and-control-resources/datcom-resources.
>
> A version of your simplification is given as equation 4.4.1.a, followed by
> an exposition on how to correct it. This takes up over 100 pages.

He, he,  just to be a little pedantic..

it's not my simplification and only about 20 pages are devoted to the
subsonic flight region, the transonic takes about 1 page and admits a lack
of understanding in this area and section C is supersonic stuff which is a
much more complex region which we will ignore for now. And then a bunch of
tables and graphs showing the results for each section,  some really good
data to help create/tailor the aero coefficients. So the problem is not
all that daunting and thank you for the excellent reference source.

The goal is to provide a reasonable set of stick force numbers that can be
fed to a control loading system (hydraulic, electrical, pnuematic,
whatever) that will give the pilot a good feel for what the aircraft is
doing within the subsonic speed envelope; i.e., < M=0.9


> Hard coding this would be not a good idea - much better to add  code to
> JSBsim so that it can be built up with parameters from the XML file  in
> the
> same way as the main body forces (Lift, Drag etc).
>
Agree, that's the idea, the calcs are in JSBSim the data is loaded in from
xml files

John



------------------------------------------------------------------------------
Create and publish websites with WebMatrix
Use the most popular FREE web apps or write code yourself; 
WebMatrix provides all the features you need to develop and 
publish your website. http://p.sf.net/sfu/ms-webmatrix-sf
_______________________________________________
Flightgear-devel mailing list
Flightgear-devel@lists.sourceforge.net
https://lists.sourceforge.net/lists/listinfo/flightgear-devel

Reply via email to