NASA NTRS · 19820016982
Recent developments in transonic Euler flow over a circular cylinder
Abstract
Numerical solutions to the Euler equations for transonic flow over a circular cylinder indicate that the inviscid flow separates ahead of the rear stagnation point. This phenomenon and various solutions related to this subject are discussed.
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Salas, M. D.. 1982-04-01. Recent developments in transonic Euler flow over a circular cylinder. https://ntrs.nasa.gov/citations/19820016982
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