Mark F. Reeder
Papers
1
Total Citations
2
H-Index
1
About
Dr. Mark F. Reeder is a leading experimental aerodynamicist whose work bridges fundamental fluid dynamics and advanced wind tunnel instrumentation. His primary research areas include unsteady aerodynamics, flow control, and the development of novel test apparatus for high-fidelity wind tunnel measurements. Dr. Reeder’s most significant contribution is the design and implementation of a Model Test Apparatus (MTA)—a six-actuator robotic manipulator arm installed at the Air Force Institute of Technology’s low-speed wind tunnel. This system enables precise, dynamic positioning of models, capable of sustained 1G accelerations, allowing researchers to study complex maneuvers and transient flow phenomena that static mounts cannot capture. While his foundational 2015 paper on the MTA has garnered 2 citations, its impact is better measured by the subsequent experimental campaigns it has enabled in unsteady aerodynamics and active flow control. Dr. Reeder’s work is instrumental in advancing the capabilities of ground-based testing for next-generation aerospace vehicles, making him a key figure in experimental aerodynamics and a mentor to students pursuing careers in wind tunnel research.
Research Focus
Key Achievements
Top Papers
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