Timeline for What specific improvements were made in supercritical airfoil design from 1980 - 2000?
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6 events
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Nov 19, 2022 at 9:11 | comment | added | Peter Kämpf | Nothing in the linked article contradicts what I said. It is only selective in what is reported. Also revealing it its way: The achievement by Vickers with their VC-10 wing is not credited, although it was the best of its time. BTW, Figure 8 demonstrates a lack of understanding what drives maximum subsonic lift. I'm not impressed. | |
Nov 19, 2022 at 4:32 | comment | added | interested22 | Though I will say, I don't disagree that there have been some conflicts between Bremen and the UK teams in the past. I interviewed an aerodynamicist from Airbus currently and he talked about the big fight over including variable-camber on the A340 wing (eventually it was not included). The A340 wing was also a competition between Bremen and the HSA team. | |
Nov 19, 2022 at 4:31 | comment | added | interested22 | Do you have a source for this? I'm pretty sure J.A. Jupp and Dykins would disagree with this. See this lecture on their A310 design efforts - they depict the airfoil as a natural development of Pearcey's "Peaky" airfoils that were used on the A300: jstor.org/stable/2398246?seq=11#metadata_info_tab_contents | |
Nov 9, 2022 at 14:30 | comment | added | Peter Kämpf | Basic work on transsonic airfoils was performed as early as 1940 by K. A. Kawalki in Germany when it was found that inverted airfoils performed better at transsonic speed. Also, the A310 wing is based on a design by Airbus Bremen which was proposed after the Hawker Siddeley design for the A310 wing proved to be mediocre. To save face, Hawker Siddeley used the Bremen design and sold it as their own. Next, the US sued Airbus for patent infringement when the A310 came out with its supercritical wing, only to lose the case because of the earlier work by Kawalki. | |
Nov 8, 2022 at 14:12 | vote | accept | interested22 | ||
Nov 8, 2022 at 14:12 | history | answered | interested22 | CC BY-SA 4.0 |