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This volume contains the description of an EC-sponsered program to
study all relevant aspects of shock/ boundary-layer interaction
control, the latter designed to improve aircraft performance at
design (cruise) and off-design conditions. The work being presented
includes a discussion of basic control experiments and the
corresponding physical modeling, to account for shock control and a
discussion of the airfoil experiments conducted for code validation
and control assessment, in conjunction with the basic experiments
and computations. The contents is comprised of a section giving a
broad overview of the research carried out here and more detailed
individual contributions by the participants in the research.
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