In this paper, we propose a two-stage regression approach, which is based on the residual correction concept.
It is based on the "iterative residual correction" concept that is successfully used for transonic wing design and subsonic multi-lifting surface design.
Additionally, the cost estimate to maintain the constellation in the regions of zero and minimum relative radial acceleration or keeping a rigid configuration is computed with the use of the residual acceleration concept.
In view of the still unproven decisively intensive "statin as monotherapy" strategy and "residual risk" concept, it is logical to ask whether other strategies, particularly fibrate/statin combination therapy, could be more beneficial and safer.
Alas, until now the bitterest comparator for the "intensive" statin monotherapy was 'usual-dose" statin monotherapy... then, in view of the lack of a proven effect of the current intensive "statin as monotherapy" strategy and "residual risk" concept, it is logical to ask whether other strategies could be more beneficial and safer [ 10].
An inverse design method based on the residual-correction concept has been developed and applied to aerodynamic design of wings for Japanese supersonic transport.
Furthermore, We present results using the modelied constitutive theoresidual sceNAPLo involving NAPL imbibition and drainage.
An alternative magnetic residual ion removal concept with in-line ion dumps for the ITER neutral beam system is presented.
To prevent the vorticity from entering the solid body, we introduce a concept residual circulation in a sense that only a partial circulation of the vortex sheet is diffused into the flow field; the rest remains at the wall.
At an aggregate level, regression diagnostics amount to analysis of inconsistency, with index plots of leverages and residuals [ 26], concepts like node-splitting [ 8], and design-by-treatment interaction [ 12, 13].
We use the concepts of residual and unknown risks in classifying the risk space.
