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20 MW Semi-Elliptical 8-foot high-temperature structures Aeronaut aerothermal testing Ames 20 MW angle of attack beneath the tile boundary layer cavity floor cavity heating rates Charred Nomex/RTV bond closed cavity flow covered with SIP displacement thick double lost-tile cavities double-tile cavity downstream wall dynamic pressure edge of tile eroded figure 13 floor of cavity flow separation free shear layer free-stream Mach number high-temperature structures tunnel Hypersonic Langley 8-foot high-temperature Langley Research Center layers of RTV length-to-depth ratio location Q maximum surface temperature mullite tile NASA TN Nomex SIP normal surface heating number of 6.6 number per meter open cavity flow Posttest primary structure reference 11 Reynolds number Riemann Zeta Function separated flow attached shear stress shuttle entry single-tile cavity space shuttle strain isolator stream structural skin surface insulation RSI temperature histories Temperature response tests were conducted thermal protection system thermal response thermocouple Turbulent Flow