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- seams a reasonable value for the height (3 times the airfoil chord b) File:Airfoil airflowl.png This is of course a very rough approximation. In reality...375 KB (64,524 words) - 20:05, 1 February 2023
- Talk:Lockheed Martin RQ-170 Sentinel/Archive 1 (section File:RQ-170 in Iran.png Nominated for speedy Deletion)including Wikipedia, and you can buy the plans for the Ho-IX / Go-229: airfoils, structure, everything, at www.albentley-drawings.com . The RQ-170 is obviously...36 KB (4,999 words) - 08:04, 12 April 2024
- velocity relative to the airfoil, and it is the standard approach to use that relative velocity to calculate the force on an airfoil based on Angle_of_attack...109 KB (17,452 words) - 09:35, 29 March 2021
- whereas those other airfoils are not. In the body, I have changed the awkward language there. it's appropriate to point to airfoils attached to sailing...73 KB (11,205 words) - 01:59, 25 March 2023
- frontal area only goes up linearly with the length, assuming a constant airfoil) so the drag at a given weight and constant speed goes up with m 1 / 2...65 KB (9,880 words) - 17:11, 30 January 2023
- know all about the stall being a function of the angle of attack of the airfoil, to the relative wind. That is why a plane can enter a "high speed stall...155 KB (22,315 words) - 12:56, 15 May 2022
- rotortip vortices, which are a 'marginal', 'tangential' phenomenon like with airfoils? --HilmarHansWerner (talk) 18:26, 5 February 2013 (UTC) could somebody...108 KB (15,300 words) - 23:08, 30 January 2023
- industry has begun using seemingly insignificant refinements in blade airfoil shapes to increase annual energy output from 10 to well over 25 percent...228 KB (33,636 words) - 01:32, 4 February 2023