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NASA NTRS · Conference Paper
Analytic prediction of dynamic stall characteristics.
Attribution
This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.
Abstract
Verbatim from NASA NTRS. Not paraphrased, not summarized.
A new approach is presented for solving the problem of predicting dynamic stall characteristics. In this approach, the unsteady aerodynamic characteristics are related theoretically to static aerodynamic characteristics which are readily available for a great number of airfoil shapes. Using these static experimental data as an input, the developed analytical method predicts dynamic stall characteristics that are in good agreement with available experimental data. The analysis is also extended to include frequency and amplitude modulation effects.
Authors
- Ericsson, L. E.
- Reding, J. P. Lockheed Missiles and Space Co., Inc.
Citation: Ericsson, L. E., Reding, J. P. (2019). Analytic prediction of dynamic stall characteristics.. Legacy CDMS. NASA NTRS ID 19720050394. https://ntrs.nasa.gov/citations/19720050394 ↗