AIREX: Effects of surface cooling and of roughness on the heating (including transition) to the windward plane-of-symmetry of the shuttle orbiter

タイトル	Effects of surface cooling and of roughness on the heating (including transition) to the windward plane-of-symmetry of the shuttle orbiter
本文（外部サイト）	http://hdl.handle.net/2060/19770016229
著者（英）	Galanski, S. R.; Bertin, J. J.; Idar, E. S., III
著者所属（英）	Texas Univ.
発行日	1977-04-01
言語	eng
内容記述	The theoretical heat-transfer distributions are compared with experimental heat-transfer distributions obtained in Tunnel B at AEDC using a 0.0175 scale model of the space shuttle orbiter configuration for which the first 80% of the windward surface was roughened by a simulated tile misalignment. The theoretical solutions indicate that thinning the boundary layer by surface cooling increased the nondimensionalized value of the local heat-transfer coefficient. Tile misalignment did not significantly affect the heat-transfer rate in regions where the boundary layer was either laminar or turbulent.
NASA分類	SPACE TRANSPORTATION
レポートNO	77N23173 AER-77-002 NASA-CR-151337
権利	No Copyright
URI	https://repository.exst.jaxa.jp/dspace/handle/a-is/182405