Code Comments
Programming Forum and web based access to our favorite programming groups.I have equations in terms of aerodynamic coefficients and these are greater than the equations itself. Now, there is some experimental data of these coefficients CL, CM, Cn etc etc in terms of the control variables that I have to find out ultimately. But this data is very limited , its is at few values and that too the other variable inputs kept zero. Say rudder deflection of my model is varied but the other control surface deflections like aileron and elevator is zero throughout. So I don't have any functional form , neither do I have the data at evry possible combination of the the variables I have to findout finally. Even the interpolation through which I can predict the value of some aerodynamic coefficients at some combination of control surface deflection will be on an assumption andI have no way to verify whtehr such a thing is correct or not. Hopefully I am clear. Vinsing Undergrad Aero Engg IITK, India Rajeev wrote: > > > Vineet Singh wrote: > greater > equations at > some but > I > > May I suggest re-posting more clearly ? You say both that > > "no. of equations is equal to no. of variables" > > and > > "variables are greater than the no. of equations" > > This is confusing. > > Variables seem to depend on control variables. What do control > variables depend on ? > > -rajeev- > >
Post Follow-up to this messagePowered by vBulletin
Copyright 2000-2006 Jelsoft Enterprises Limited.