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An analytical treatment of the "strong" interaction problem in hypersonic viscous flow on a noninsulated flat plate is presented, using the method of "similar" solutions of the compressible boundary layer equations. Recent experimental data which confirm some of the theoretical results are also discussed. 1 2 yi(w-local heat transfer coefficient Ch.= p.uHG Rex i Po UX free stream Reynolds number on the Rex 9 .0basis of x A,B,C,D defined in Eqs 16-19 .w exponent in the viscosity law Subscripts 'o", I1', wo", aw" refer, respectively, to the stagnation conditions, the conditions at the edge of the boundary layer, the conditions in the free stream, and the conditions on the surface.

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