Recent advances and challenges in the generation of reduced order aerodynamic models
using computational fluid dynamics are presented. The models reviewed are those that can …

An approach for the generation of aerodynamic tables using computational fluid dynamics is
discussed. For aircraft flight dynamics, forces and moments are often tabulated in multi …

The generation of reduced-order models for computing the unsteady and nonlinear
aerodynamic loads on an aircraft from pitching motions in the transonic speed range is …

TRADITIONALLY, the prediction of aerodynamic character-istics of an airplane during the
conceptual design stage relies on handbook methods or linear fluid mechanics assumptions …

This article is focused on the design of forced motions and developing models that can
accurately and rapidly predict the aerodynamic stability derivatives of air vehicles over a …

Modeling nonlinear unsteady aerodynamic effects in the simulation of modern fighter aircraft
is still a very challenging task. A framework for approximating nonlinear unsteady …

The challenges in the modeling of the unsteady lift of a two-dimensional NACA 0012 airfoil
oscillating and translating at large incidence angles are investigated in this paper. Forced …

HISTORICALLY, stability and control (S&C) engineers have used an iterative process
combining semiempirical lowerorder, wind-tunnel, and flight-test modeling techniques to …

I completed my MSc Thesis in collaboration with the Royal Netherlands Aerospace Centre
(NLR), in Amsterdam from November, 2023, to September, 2024. As the leading …

As aircraft are increasingly specialized for low-observability and maneuverability, the
aerodynamic identification process has become increasingly important. Recently, the …