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NASA NTRS ยท 19780011848

Viscous flow simulations in VTOL aerodynamics

Abstract

The critical issues in viscous flow simulations, such as boundary-layer separation, entrainment, turbulence modeling, and compressibility, are discussed with regard to the ground effects problem for vertical-takeoff-and-landing (VTOL) aircraft. A simulation of the two-dimensional incompressible lift jet in ground proximity is based on solution of the Reynolds-averaged Navier-Stokes equations and a turbulence-model equation which are written in stream function-vorticity form and are solved using Hoffman's augmented-central-difference algorithm. The resulting equations and their shortcomings are discussed when the technique is extended to two-dimensional compressible and three-dimensional incompressible flows.

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BibTeXRIS

Bower, W. W.. 1978-02-01. Viscous flow simulations in VTOL aerodynamics. https://ntrs.nasa.gov/citations/19780011848

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