NASA NTRS · 19880035065
Numerical simulation of wing lift augmentation with spanwise tip blowing
Abstract
Navier-Stokes simulations are used to study the phenomena of wing lift augmentation with spanwise tip blowing. Flowfields calculated for varying blowing conditions are analyzed to determine the mechanisms responsible for providing lift augmentation. It is found that both viscous and inviscid effects are important.
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Caruso, S. C., Mendenhall, M. R., Childs, R. E.. 1988-01-01. Numerical simulation of wing lift augmentation with spanwise tip blowing. https://ntrs.nasa.gov/citations/19880035065
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