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Showing 1 to 2 of 2 for “"Stratford Pressure Recovery"”.
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Shape optimization of cambered airfoils using a genetic algorithm and a multipoint inverse method
… Liebeck L1003 airfoil, which was designed with a Stratford pressure recovery distribution. In the third study, a series of Clmax optimization runs was performed for varying pitching moments at Re = 6.00 * 10^6, revealing final solutions that segregated into two types of airfoils that differ in …
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Airfoil design framework for optimized boundary-layer integral parameters
Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-04-12 without embargo terms