1. Recovery temperatures and heat transfer near two-dimensional roughness elements at Mach 3.1;Brinich;NACA TN 4213,1958
2. Measurement of heat transfer in bubbles of separated flow in supersonic air streams;Naysmith,1961
3. Measurement of heat transfer in bubbles of separated flow in supersonic air streams;Naysmith,1961
4. Laminar heat transfer to a two-dimensional backward-facing step from the highenthalpy supersonic flow in the shock tube;Rom;AIAA Jl,1964
5. Measurements of heat transfer and recovery temperature in a separated flow at a Mach number of 1.8;Thomann;F.F.A. Rep. 82,1959