Michael H. Durham

TL;DR: Results obtained from a second wind tunnel test of the first model in the Benchmark Models Program are described, which consisted of a rigid semispan wing having a rectangular planform and a NACA 0012 airfoil shape which was mounted on a flexible two degree of freedom mount system.

TL;DR: In this article, the authors present a roadmap for scalable, on-demand, distributed air mobility technologies for vehicle and airspace systems based on the Small Aircraft Transportation System (SATS).

TL;DR: The Benchmark Active Controls Technology (BACT) model is a part of the Benchmark Models Program (BMP), a NASA Langley Research Center program that includes a series of models which were used to study different aeroelastic phenomena and to validate computational fluid dynamics codes.

TL;DR: An experimental effort was implemented in aeroelasticity called the Benchmark Models Program, which focuses on increasing the understanding of the physics of unsteady flows and providing data for empirical design.

TL;DR: In this paper, the authors present a status report on an active control flutter model, which is currently in the design and fabrication phase and is part of the Benchmark Models Program (BMP).