INVERSE PROBLEMS OF HEAT AND MASS TRANSFER ON HYPERSONIC AIRCRAFTS PERMEABLE SURFACES. V. MIXED PROBLEMS FOR THE FRAGMENTS OF SEGMENT OF CONTROL
The problems of mathematical modeling of effective control of heat and mass transfer and friction in laminar boundary layer on permeable cylindrical and spherical surfaces of hypersonic aircraft are considered. Mixed problems are formulated for fragments of segment of control. Questions of proximity in mixed problems are discussed. A scheme of algorithm for choosing the variant of the problem being solved is given.