Characterization of Unsteady Pressures on a Blunt Trailing Edge Using a Direct-Mount Pressure Scanner
Author:
Affiliation:
1. Resono Pressure Systems, LLC
2. University of Wyoming, Laramie
3. TE Connectivity Company
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1827
Reference8 articles.
1. Unsteady Surface Pressure Reconstruction on an Oscillating Airfoil Using the Wiener Deconvolution Method
2. Wiener Deconvolution for Reconstruction of Pneumatically Attenuated Pressure Signals
3. Experimental Investigation of Base-Drag Reduction via Boundary-Layer Modification
4. Experimental investigation on the influence of boundary layer thickness on the base pressure and near-wake flow features of an axisymmetric blunt-based body
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