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OVERFLOW results for the Juncture Flow Experiment

Speaker: Henry Lee, Science and Technology Corporation/NASA Advanced Supercomputing Division, NASA Ames Research Center

Presentation

Seminar Slide Deck (PDF-71.7MB)

Abstract

The presentation focuses on the CFD analysis done in support of NASA's Juncture Flow Experiment (under NASA’s Transformational Tools and Technologies Project (T3). The first phase of the Juncture Flow experiment, performed in NASA Langley’s 14- by 22-Foot Subsonic Tunnel, has been completed. Comparisons between OVERFLOW CFD simulations and wind tunnel experimental results will be shown. Oil flow results, surface pressure cuts, velocity profiles, and Reynolds stress profiles will be compared. Preliminary results analyzing the effect of grid resolution, wind tunnel walls, and turbulence models on the Juncture flow region will be presented. The results are not meant to be a validation study, but more as a preliminary evaluation of the current status of Reynolds averaged Navier-Stokes (RANS) CFD simulations.

Biography

Photo of Henry Lee
Henry Lee is an aerospace engineer with Science and Technology Corporation, working with both the SLS group at NASA Ames Research Center and the Juncture Flow experiment design committee in the Computational Aerosciences Branch of the NASA Advanced Supercomputing Division. He obtained his Bachelors from University of California, San Diego in 2007, and his Masters in Aeronautics/Astronautics Engineering from Stanford University in 2009.