This paper reviews several decades' worth of research on the topic of slat noise arising from
high-lift systems of commercial aircraft. A high-lift system is commonly used for providing …

The leading edge slat of a high-lift system is one of the main noise contributors on many
commercial aircraft during approach. This paper continues our previous studies on the gap …

Mechanical instabilities and elastic nonlinearities are emerging means for designing
deployable and shape adaptive structures. Dynamic snap-through buckling is investigated …

Transport class aircraft produce a significant amount of airframe noise during approach and
landing due to exposed geometric discontinuities that are hidden during cruise. The leading …

The leading edge slat of a high-lift system is one of the main contributors to airframe noise
during approach. In a previous experimental study, we assessed the performance of an …

Fluid-structure interaction (FSI) analysis is a common tool used to analyze aeroelastic
problems. The traditional FSI scheme couples independent structure and fluid solvers in …

A coupled kinetic Monte Carlo–Finite Element Analysis (kMC–FEA) method is developed
with a numerical implementation in the Scalable Implementation of Finite Elements at NASA …