Journal of Aircraft · 1992 · 88 citations · 27 references
Threedimensional ConfigurationsEngineeringAerospace EngineeringAerodynamic DesignMultidisciplinary Design OptimizationAerodynamic Shape DesignDesignMechanical SystemsShape OptimizationSystems EngineeringAerodynamicsNavier-stokes EquationsStructural OptimizationComputational MechanicsAdjoint Operator/control TheoryAircraft Design ProcessAerostructure
Few aerodynamic shape design concepts have been surveyed and classified, with adjoint operator/control theory emerging as a promising interdisciplinary approach for high‑dimensional design. Future research will focus on applying Navier‑Stokes equations to three‑dimensional configurations, emphasizing interdisciplinary constrained optimization and the development of adjoint/control theory. The study outlined the positive and negative characteristics of the most prominent aerodynamic shape design methods.
A limited number of aerodynamic shape design concepts have been surveyed and an attempt has been made to classify them. Characteristics, both positive and negative, of the more prominent methods were outlined. Future research is expected to concentrate on the use of Navier-Stokes equations and applications to threedimensional configurations. Interdisciplinary constrained optimization is expected to play a more prominent role in the immediate future. Adjoint operator/control theory and its variations are the most promising concepts for interdisciplinary aerodynamic shape design which involves a large number of variables. This theory is expected to constitute the major development area in future research.
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Aerodynamic design via control theory
Antony Jameson · Journal of Scientific Computing · 1988 · 1.9K citations
Two-dimensional transonic aerodynamic design method
Michael B. Giles, Mark Drela · AIAA Journal · 1987 · 188 citations