In the past few Sears there has been interest in using response surface tec
hniques to create surrogates to computer simulations. Response surface tech
niques allow detection and correction of errors as well as filtering out nu
merical noise, but these techniques introduce additional modeling errors. M
ethods of reducing both noise and modeling errors are explored. It is also
demonstrated that repairing designs with large errors is preferable to elim
inating these designs from consideration. Response surface approximations f
or a high-speed civil transport wing weight equation created from the resul
ts of a large number of structural optimizations are used for demonstration
. It is shown that the statistical tools available for response surface tec
hniques are effective for error detection and for filtering out noise. Once
the noise is reduced, modeling errors can also be reduced by increasing th
e order of the approximation.