This work considers the design optimization of a flapping wing in forward flight with active
shape morphing, aimed at maximizing propulsive efficiency under lift and thrust constraints …

This paper presents a novel multidisciplinary framework for performing shape and topology
optimization of a flexible wing structure. The topology optimization is integrated into a …

An overview of the deployment of multidisciplinary-optimization technologies in an industrial
environment is presented herein. This capability is being developed in a multilevel …

The design of satellites and their operation is a complex task that involves a large number of
variables and multiple engineering disciplines. Thus, it could benefit from the application of …

Preliminary aircraft design studies use structural weight models that are calibrated with data
from existing aircraft. Computing weights with these models is a fast procedure that provides …

WITH the advent of multidisciplinary design optimization (MDO), designers have started to
integrate various disciplines in the aircraft design process. The strong coupling between …

The airfoil design problem, in which an engineer seeks a shape with desired performance
characteristics, is fundamental to aerodynamics. Design workflows traditionally rely on …

Formulating conceptual-stage aircraft design problems as geometric programs, which are a
specific type of convex optimization problem, is proposed. Recent advances in convex …

The adoption of conventional “black metal” composites in aircraft structures has lead to an
improvement in performance over previous metallic designs. With the maturation of …

Electrified aircraft benefit from the versatile ways electric motors can be integrated with an
airframe. However, thermal management is needed to move waste heat out of the motors …