NASA NTRS · 19870035209
Vortical flow aerodynamics - Physical aspects and numerical simulation
Abstract
Progress in the numerical simulation of vortical flow due to three-dimensional flow separation about flight vehicles at high angles of attack and quasi-steady flight conditions is surveyed. Primary emphasis is placed on Euler and Reynolds-averaged Navier-Stokes methods where the vortices are 'captured' as a solution to the governing equations. A discussion of the relevant flow physics provides a perspective from which to assess numerical solutions. Current numerical prediction capabilities and their evolutionary development are surveyed. Future trends and challenges are identified and discussed.
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Newsome, Richard W., Kandil, Osama A.. 1987-01-01. Vortical flow aerodynamics - Physical aspects and numerical simulation. https://ntrs.nasa.gov/citations/19870035209
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