Three-dimensional hypersonic flow of viscous gas in chemical disequili
brium around blunt bodies is investigated. A method is proposed for so
lving such three-dimensional problems by means of two-dimensional solu
tions applicable with arbitrary Reynolds numbers for real gas properti
es. The method is based on similarity relations expressing the heat fl
ux, friction, and concentration of the components at the surface of an
axisymmetric body. The accuracy of the similarity relations is estima
ted by finite-difference calculations of the three-dimensional equatio
ns of the Viscous shock layer for bodies of various shapes entering th
e Earth's atmosphere along planned trajectories. Various models of cat
alytic surface activity are considered.