Princeton Dynamic Stall Database: Upward ramp-type pitching motions

Kiefer, Janik; Brunner, Claudia E.; Hansen, Martin O. L.; Hultmark, Marcus
Issue date: 2022
Rights:
Creative Commons Attribution 4.0 International (CC BY)
Cite as:
Kiefer, Janik, Brunner, Claudia E., Hansen, Martin O. L., & Hultmark, Marcus. (2022). Princeton Dynamic Stall Database: Upward ramp-type pitching motions [Data set]. Princeton University. https://doi.org/10.34770/b3vq-sw14
@electronic{kiefer_janik_2022,
  author      = {Kiefer, Janik and
                Brunner, Claudia E. and
                Hansen, Martin O. L. and
                Hultmark, Marcus},
  title       = {{Princeton Dynamic Stall Database: Upward
                 ramp-type pitching motions  }},
  publisher   = {{Princeton University}},
  year        = 2022,
  url         = {https://doi.org/10.34770/b3vq-sw14}
}
Description:

This data set contains data of a NACA 0021 airfoil as it undergoes upward ramp-type pitching motions at high Reynolds numbers and low Mach numbers. The parametric study covers a wide range of chord Reynolds numbers, reduced frequencies and pitching geometries characterized by varying mean angle and angle amplitude. The data were acquired in the High Reynolds number Test Facility at Princeton University, which is a closed-loop wind tunnel that can be pressurized up to 23 MPa and allowed for variation of the chord Reynolds number over a range of 5.0 × 10^5 ≤ Re_c ≤ 5.5 × 10^6. Data were acquired using 32 pressure taps along the surface of the airfoil. The data are the phase-averaged results of 150 individual half-cycles for any given test case.

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