NASA NTRS ยท 19910012782
Numerical simulation of swept-wing flows
Abstract
The transition process characteristics of flows over swept wings were computationally modelled. The crossflow instability and crossflow/T-S wave interaction are analyzed through the numerical solution of the full three dimensional Navier-Stokes equations including unsteadiness, curvature, and sweep. The leading-edge region of a swept wing is considered in a three-dimensional spatial simulation with random disturbances as the initial conditions.
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Reed, Helen L.. 1991-02-01. Numerical simulation of swept-wing flows. https://ntrs.nasa.gov/citations/19910012782
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