The advent of Urban Air Mobility (UAM) has necessitated a paradigm shift in aircraft design
from traditional regression methods to physics-based analysis and the use of modern …

Transonic flow fields are marked by shock waves of varying strength and location and are
crucial for the aerodynamic design and optimization of high-speed transport aircraft. While …

In the early stages of aerospace design, reduced-order models (ROMs) are crucial for
minimizing computational costs associated with using physics-rich field information in many …

To facilitate the structural design of an aircraft wing, we propose a simulation technique that
can not only readily reshape a wing structure, but also rapidly yet accurately analyze its …

Exploring the behavior of complex industrial problems might become burdensome,
especially in high-dimensional design spaces. Reduced Order Models (ROMs) aim to …

Surrogate model is an efficient tool to replace the high-fidelity (HF) simulations governed by
partial differential equations (PDEs) to obtain response under different parameters (eg …

This paper uses a polynomial controller with non‐linear performance that is a summation of
polynomials in non‐linear states. The optimal performance of this controller depends to a …

This work aims to identify key barriers to the widespread adoption of high-performance
computing (HPC) and develop a framework to help new users onboard to HPC resources …

Aircraft design optimization traditionally relies on computationally expensive simulation
techniques such as Finite Element Method (FEM) and Finite Volume Method (FVM), which …

To facilitate the structural design of an aircraft wing, we propose a simulation technique that
can not only readily reshape a wing structure, but also rapidly yet accurately analyze its …