Efforts to eliminate mistakes in and descrepancies between the different methods in aerodynamics,
Illustrated by two test cases focussing on refined wing root design
DLR-F5: Design of an experiment: including a wing and its flow boundary |
DLR-F5: Experimental results in the Göttingen Transonic Windtunnel (TWG) |
DLR-F9: Larger model with cropped wings for measuring refined flow details |
DLR-F9: Geometry of cropped wings aircraft in TWG for CFD simulation |
2015