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タイトルPrediction of boundary-layer characteristics of an oscillating airfoil
著者(英)Carr, L. W.; Cebeci, T.
著者所属(英)California State Univ.|Army Aviation Research and Development Command|NASA Ames Research Center
発行日1981-01-01
言語eng
内容記述The evolution of unsteady boundary layers on oscillating airfoils is investigated by solving the governing equations by the Characteristic Box scheme. The difficulties associated with computing the first profile on a given time line, and the velocity profiles with partial flow reversal are solved. A sample calculation is performed for an external velocity distribution typical of those found near the leading edge of thin airfoils. The viability of the calculation procedure is demonstrated. Previously announced in STAR as N81-28391
NASA分類AERODYNAMICS
レポートNO83A46435
権利Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/402430


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