File:Effect of sweep angle on dynamic stall for lift coefficient.jpg
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Summary
| Description |
English: Effect of sweep angle on dynamic stall for lift coefficient |
| Date | |
| Source | The influence of sweep on the aerodynamic loading of an oscillating NACA 0012 airfoil. Volume 1: Technical report |
| Author |
St.hilaire, A. O. Carta, F. O. Fink, M. R. Jepson, W. D. |
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This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.) |  |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 16:58, 17 June 2021 | | 4,544 × 6,298 (1.31 MB) | HybridCFD | Uploaded a work by St.hilaire, A. O. Carta, F. O. Fink, M. R. Jepson, W. D. from The influence of sweep on the aerodynamic loading of an oscillating NACA 0012 airfoil. Volume 1: Technical report with UploadWizard |
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