Normal
0
21
false
false
false
MicrosoftInternetExplorer4
I found
that many certified LSA aircrafts and some standard FAR 23 certified don't have
mass-balanced surfaces. I'm interested in how they are designed to show freedom
from flutter, especially control surface flutter and if these aircrafts can
handle a disconnected freefloating surface emergency (due to cable failure, for
example).
If they are
not prone to develop flutter in normal operation, how things may change if, for
example, the aileron cable fails?
/* Style Definitions */
table.MsoNormalTable
{mso-style-name:"Tabel Normal";
mso-tstyle-rowband-size:0;
mso-tstyle-colband-size:0;
mso-style-noshow:yes;
mso-style-parent:"";
mso-padding-alt:0cm 5.4pt 0cm 5.4pt;
mso-para-margin:0cm;
mso-para-margin-bottom:.0001pt;
mso-pagination:widow-orphan;
font-size:10.0pt;
font-family:"Times New Roman";
mso-ansi-language:#0400;
mso-fareast-language:#0400;
mso-bidi-language:#0400;}