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Start Over Author "Lockard, David P." Journal journal of aircraft
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2. Wing-tip vortex calculations using a high-accuracy scheme

Author

Lockard, David P. and Moris, Philip J.

Subjects
Airplanes -- Wings, Sound -- Observations, Aerospace and defense industries, Business, Science and technology
Abstract

The steady flow calculations over a finite wing were performed using the high-order spatial operators of a computational aeroacoustics (CAA) scheme, as well as a time-marching algorithm. The equations of motion in three dimensions are provided, and there is emphasis on three-dimensional results for low-speed flow over a NACA 0012 wing. Vortex growth was larger than in experimental measurements, although other parameters were well predicted.

Published
1998

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