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8-foot high-temperature structures acoustic baffles aerodynamic heating Aerothermal 1145 aerothermal performance aerothermal tests allowed for thermal angle of attack arcing bolted CM CM CM cooling corrugation-stiffened skin corrugations deflectometer differential pressure drag support frequencies Glasrock high-temperature structures tunnel hot gas flow hypersonic inconel foil insulation package L-shaped clip Langley 8-foot high-temperature Langley Research Center leading edge leading-edge fairing located metallic thermal protection NASA TN obtained panel holder panel surface preheat prevent hot gas radiant and aerothermal radiant lamps seam welded shingle-slip joint supports shown in figure side-edge seals skin and supports spot welded standoffs static-load deflection stiffeners stream structural integrity subjected to 32 SUPERALLOY surface temperature temperature distributions temperature histories temperature time histories test panel test series thermal analysis thermal cycle thermal expansion thermal insulation thermal protection system thermocouple titanium sheet TPS cavity TPS was subjected U.S. Customary Units unit Reynolds number vehicle primary structure wind tunnel