Timeline for What would the density profile of this shock wave look like, roughly?
Current License: CC BY-SA 3.0
9 events
| when toggle format | what | by | license | comment | |
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| Jun 17, 2020 at 8:28 | history | edited | CommunityBot |
Commonmark migration
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| Aug 31, 2017 at 22:06 | vote | accept | uhoh | ||
| Aug 31, 2017 at 18:16 | answer | added | GSammons | timeline score: 5 | |
| Jul 9, 2017 at 14:04 | history | tweeted | twitter.com/StackAviation/status/884050558687916032 | ||
| Jul 9, 2017 at 13:05 | comment | added | mins | Another pressure distribution graph (middle) at the end of this article. | |
| Jul 9, 2017 at 12:48 | comment | added | uhoh | @mins very nice! So pretty much something like either the first or the third curve in my example guesses. As the video caption explains, it's like a simple transition from one index of refraction to another. I've just got to generate it in 3D (make a cone around the engine axis) and see what happens. I can always add a transition thickness of a millimeter or centimeter and see if that changes the appearance.Thanks! | |
| Jul 9, 2017 at 12:47 | comment | added | mins | Not an answer, but this document shows an abrupt transition. | |
| Jul 9, 2017 at 12:33 | history | edited | uhoh | CC BY-SA 3.0 |
added 90 characters in body
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| Jul 9, 2017 at 12:25 | history | asked | uhoh | CC BY-SA 3.0 |
