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S Nov 11 at 14:04 history bounty ended CommunityBot
S Nov 11 at 14:04 history notice removed CommunityBot
Nov 4 at 19:18 history edited Camille Goudeseune CC BY-SA 4.0
edited title
S Nov 3 at 13:02 history bounty started Apoorva Shukla
S Nov 3 at 13:02 history notice added Apoorva Shukla Draw attention
Jun 15, 2019 at 12:00 history tweeted twitter.com/StackAviation/status/1139865297211576321
May 31, 2019 at 12:28 vote accept Aerocurios
May 28, 2019 at 14:20 comment added Aerocurios Yeah, I read the source and the first coefficient is actually negative. Also, yeah, I wish the transition from the sharp cone to the cylinder was smoother here.
May 28, 2019 at 13:53 comment added bukwyrm About that image: a) Is the first coeficient really meant to be negative? ----- b) the graph shows no noses that are both sharp-tipped and smooth-walled, so they do not really support your question - #2 and #4 differ in tip and wall
May 28, 2019 at 1:36 answer added Koyovis timeline score: 5
May 27, 2019 at 22:55 history edited Aerocurios CC BY-SA 4.0
added 69 characters in body
May 27, 2019 at 22:43 history edited Aerocurios CC BY-SA 4.0
added 69 characters in body
May 27, 2019 at 18:14 answer added Peter Kämpf timeline score: 15
May 27, 2019 at 16:26 comment added Jihyun I didn't downvote, to be clear. I'm just saying that the answer I linked provides a very good explanation that partially clears up some conceptual questions. Any extra answers on this page should at least add to what @PeterKampf explains in his answer.
May 27, 2019 at 2:51 comment added Koyovis Not a duplicate. This question states awareness of the difference between subsonic and supersonic. It is a well stated question and does not deserve to be downvoted.
May 27, 2019 at 1:48 comment added Aerocurios The first answer mentions my first point above and the second answer mentions the second point, but writes in text that the skin friction drag is lower while supporting it with an image that says the form drag is lower. The former is supported by the erroneously wetted area argument and the latter is stated as fact without reasoning (I’ve yet to read Hoerner). Why is the form drag and skin friction drag of a blunter (maybe even hemispherical) nose smaller than for a sharper nose (even at optimal AOA) and why do gliders ignore it?
May 27, 2019 at 1:40 history edited Aerocurios CC BY-SA 4.0
added 189 characters in body
May 26, 2019 at 21:50 review Close votes
May 27, 2019 at 3:25
May 26, 2019 at 21:31 comment added Jihyun Not sure if it's a dupe, but aviation.stackexchange.com/questions/24414/… provides a pretty good explanation.
May 26, 2019 at 21:25 review First posts
May 26, 2019 at 22:15
May 26, 2019 at 21:23 history asked Aerocurios CC BY-SA 4.0