NASA NTRS · 19890010133
A computationally efficient modelling of laminar separation bubbles
Abstract
The goal is to accurately predict the characteristics of the laminar separation bubble and its effects on airfoil performance. Toward this end, a computational model of the separation bubble was developed and incorporated into the Eppler and Somers airfoil design and analysis program. Thus far, the focus of the research was limited to the development of a model which can accurately predict situations in which the interaction between the bubble and the inviscid velocity distribution is weak, the so-called short bubble. A summary of the research performed in the past nine months is presented. The bubble model in its present form is then described. Lastly, the performance of this model in predicting bubble characteristics is shown for a few cases.
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Dini, Paolo, Maughmer, Mark D.. 1989-02-01. A computationally efficient modelling of laminar separation bubbles. https://ntrs.nasa.gov/citations/19890010133
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