首页> 美国政府科技报告 >DATA REPORT FOR TESTS ON THE HEAT TRANSFER EFFECTS OF THE 0.0175-SCALE ROCKWELL INTERNATIONAL SPACE SHUTTLE VEHICLE MODEL 22-OT IN THE AEDC 50-INCH B WIND TUNNEL (OH4B) VOLUME 2 OF 3
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DATA REPORT FOR TESTS ON THE HEAT TRANSFER EFFECTS OF THE 0.0175-SCALE ROCKWELL INTERNATIONAL SPACE SHUTTLE VEHICLE MODEL 22-OT IN THE AEDC 50-INCH B WIND TUNNEL (OH4B) VOLUME 2 OF 3

机译:关于在aEDC 50英寸B风洞(OH4B)第2卷中的0.0175-sCaLE罗克韦尔国际空间梭车模型22-OT的传热效果的测试数据报告

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摘要

Results of wind tunnel heat transfer tests of 0.0175-scale Rockwell International Space Shuttle Vehicle configurations for orbiter alone, tank alone, and orbiter plus external tank are presented in this report. Body flap shielding of Sakes’ during simulated entry was also investigated.nThe tests were conducted at Mach 8 for thirteen Reynolds number per foot values ranging from 0.5 x 106 to 3.72 x 106.

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