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S Jun 11, 2021 at 6:13 history suggested Rodrigo de Azevedo
Added tags.
Jun 11, 2021 at 0:43 review Suggested edits
S Jun 11, 2021 at 6:13
Jun 1, 2021 at 9:00 history tweeted twitter.com/StackAviation/status/1399651935440060418
May 31, 2021 at 22:40 comment added quiet flyer This sentence is unclear: "For example: if I pitch the airplane up, but also increase power and am able to maintain the same speed, then no, the AoA hasn’t changed, although it may have varied in the transition between one situation and the other. " It sounds more like an answer than a question. If you don't tell us anything about the relationship between the change in pitch attitude and the change in climb angle, then it is impossible to know whether or not the angle-of-attack has changed. Only if the two values are identical, has the angle-of-attack remained constant.
May 31, 2021 at 22:34 answer added Phil Crowther timeline score: 1
Nov 9, 2018 at 0:27 answer added Robert DiGiovanni timeline score: 4
Nov 8, 2018 at 23:55 history edited Zeus CC BY-SA 4.0
Accidentally repeated paragraph
Nov 8, 2018 at 21:42 answer added DLH timeline score: 4
Nov 8, 2018 at 18:57 comment added Peter Kämpf Lift will not change when angle of attack changes and speed is adjusted accordingly to maintain level flight. What does change is the lift coefficient.
Nov 8, 2018 at 15:36 comment added quiet flyer Any question including such a poorly-drawn diagram as this, really ought not be answered at all, because it is a question with erroneous content included as part of the premise of the question. Thanks a lot, NASA!
Nov 8, 2018 at 15:24 answer added quiet flyer timeline score: 4
Nov 8, 2018 at 7:39 answer added Jan timeline score: 1
Nov 8, 2018 at 4:52 history asked Sachin Chaudhary CC BY-SA 4.0