发明名称 Method of determining laminar turbulent boundary layer impact in cryo-stream and cryo-channel
摘要 The determination method involves feeding an indicator fluid into the cryostream. This has a low impact on the model in the stream, in solid form. The boundary layer impact can then be determined with those positions at which the indicator disappears quicker under the turbulent flow than under the laminar flow. The indicator fluid is fed into the cryo-fluid as a gas. It impacts the model in crystalline form and then disappears under turbulent flow by fast sublimation. Preferably the indicator gas is fed into a cryo-channel by means of a movable lance (15). Preferably carbon dioxide is used as the indicator gas.
申请公布号 DE19641351(C1) 申请公布日期 1998.05.07
申请号 DE19961041351 申请日期 1996.10.08
申请人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V., 53175 BONN, DE 发明人 STAHL, BERNHARD, DIPL.-ING. DR., 50933 KOELN, DE
分类号 G01M9/06;(IPC1-7):G01M9/06 主分类号 G01M9/06
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