This research treats the experimental platform itself as a scientific contribution. Rather than viewing tunnels, flow generators, and test hardware as background infrastructure, the work studies how facility design, actuation strategy, optical access, manufacturability, and dynamic response shape the quality of the aerodynamic knowledge that follows. The projects include a shuttered open-jet wind tunnel for unsteady-flow generation and an additive-manufactured supersonic wind tunnel designed for both education and research. Together, they show that meaningful advances in fluid mechanics often begin with building better environments in which to ask the question.
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Advancing Flight ResearchWind Tunnel Innovation Research Diagram
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Cook, Thomas, Sidaard Gunasekaran, Michael V. Ol, and Michael P. Mongin. "Frequency Response of a Shuttered Open Jet Wind Tunnel." In AIAA Scitech 2020 Forum, p. 1760. 2020. https://doi.org/10.2514/6.2020-1760
Design and Analysis of an Additive Manufactured Supersonic Wind Tunnel
Gazella, Matthew R., Jonathon Hill, Scott Chriss, Austin J. Abel, and Sidaard Gunasekaran. "Design and Analysis of an Additive Manufactured Supersonic Wind Tunnel." In AIAA Scitech 2020 Forum, p. 1354. 2020. https://doi.org/10.2514/6.2020-1354
