COMPUTATIONAL FLUID DYNAMICS OF WHOLE-BODY AIRCRAFT

Author:

Agarwal Ramesh1

Affiliation:

1. National Institute for Aviation Research, Wichita State University, Wichita, Kansas 67260-0093; e:mail:

Abstract

▪ Abstract  The current state of the art in computational aerodynamics for whole-body aircraft flowfield simulations is described. Recent advances in geometry modeling, surface and volume grid generation, and flow simulation algorithms have led to accurate flowfield predictions for increasingly complex and realistic configurations. As a result, computational aerodynamics has emerged as a crucial enabling technology for the design and development of flight vehicles. Examples illustrating the current capability for the prediction of transport and fighter aircraft flowfields are presented. Unfortunately, accurate modeling of turbulence remains a major difficulty in the analysis of viscosity-dominated flows. In the future, inverse design methods, multidisciplinary design optimization methods, artificial intelligence technology, and massively parallel computer technology will be incorporated into computational aerodynamics, opening up greater opportunities for improved product design at substantially reduced costs.

Publisher

Annual Reviews

Subject

Condensed Matter Physics

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