TY - JOUR
T1 - Recent advances in computational aerodynamics
AU - Agarwal, Ramesh K.
AU - Desse, Jerry E.
PY - 1991/4/2
Y1 - 1991/4/2
N2 - The current state of the art in computational aerodynamics is described. Recent advances in the discretization of surface geometry, grid generation, and flow simulation algorithms have led to flowfield predictions for increasingly complex and realistic configurations. As a result, computational aerodynamics is emerging as a crucial enabling technology for the development and design of flight vehicles. Examples illustrating the current capability for the prediction of aircraft, launch vehicle and helicopter 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.
AB - The current state of the art in computational aerodynamics is described. Recent advances in the discretization of surface geometry, grid generation, and flow simulation algorithms have led to flowfield predictions for increasingly complex and realistic configurations. As a result, computational aerodynamics is emerging as a crucial enabling technology for the development and design of flight vehicles. Examples illustrating the current capability for the prediction of aircraft, launch vehicle and helicopter 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.
UR - http://www.scopus.com/inward/record.url?scp=0026413089&partnerID=8YFLogxK
U2 - 10.1016/0010-4655(91)90149-F
DO - 10.1016/0010-4655(91)90149-F
M3 - Article
AN - SCOPUS:0026413089
SN - 0010-4655
VL - 65
SP - 8
EP - 16
JO - Computer Physics Communications
JF - Computer Physics Communications
IS - 1-3
ER -