Antony Jameson pioneered CFD-based aerodynamic design optimization in the late 1980s.
In addition to developing the fundamental theory, Jameson implemented that theory in …

As a high-fidelity approach to transition prediction, the coupled Reynolds-averaged Navier–
Stokes (RANS) and linear stability theory (LST)-based e N method is widely used in …

Due to the high sensitivity of laminar wings to uncertain factors, although there have been a
lot of engineering application attempts, so far laminar flow technology has not been …

In the context of traditional aerodynamic shape optimization design methods, the necessity
to re-execute the complete optimization process when the initial shape changes poses …

The transition to turbulence induced by counter-rotating wall-normal rotating cylindrical
roughness pairs immersed within a laminar boundary layer on a flat plate is investigated …

Natural laminar-flow (NLF) wings and hybrid laminar-flow control (HLFC) wings are efficient
drag reduction technologies. It is vital to develop robust laminar-flow wings to research the …

To realize the drag reduction benefit of boundary-layer transition control strategies, it is
crucial to integrate transition prediction into the vehicle design through an optimization …

As the computational resources available to aerodynamicists increase, so does the number
of tools with which they can analyze their designs. The key skill of a good engineer is …

It is an inherent uncertainty problem that the application of laminar flow technology to the
wing of large passenger aircraft is affected by flight conditions. In order to seek a more …

View Video Presentation: https://doi. org/10.2514/6.2022-1865. vid A smooth local
correlation-based transition model is fully coupled to a RANS-based Newton-Krylov flow …