Boundary-Layer Transition and Heat Transfer in Shock Tubes
作者： R. A. HARTUNIAN , A. L. RUSSO , P. V. MARRONE
DOI: 10.2514/8.8656
关键词:
摘要: … An extended range of comparison is provided by determination of turbulent heat transfer rates from temperature records obtained in the present study. For the most part, only data …
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