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Just curious how do you use a subreddit to keep interesting bookmarks


Create your own subreddit.

Submit links to subreddit of the websites you want 'bookmark'.

Done: an online bookmark list.


Oh wow i never thought about that and the best thing is i can even share that with other people Damnn thats a good idea thanks for bringing it up man !!


Ok, I'm hijacking this thread because there's some confusion about 'limit' load.

http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgFAR.nsf...


You're not hijacking it, just adding some contextual information, namely: "Strength requirements are specified in terms of limit loads (the maximum loads to be expected in service) and ultimate loads (limit loads multiplied by prescribed factors of safety). Unless otherwise provided, prescribed loads are limit loads."


Was that an airplane joke?


Assumes the exit is on the periphery and you're not stuck on a loop (a free standing wall in the interior).


Also, that there isn't a hungry Minotaur hunting in the maze.


Why not?

Is it somehow morally reprehensible? Because it would be ineffective? Do you want the govt to see your dick pics?

I'm curious about about your flat out rejection of this proposal.


The free pdf preview seems to consolidate some of the concepts from the register machine chapters of SICP.


Off the top of my head, there are at least two more potential ways of measuring AoA: 1. Similar to your ultrasonic lattice, but using a cone of hot wire anemometers, so that each wire is set at an offset angle to the 'zero' direction. As the AoA changes relative to the cone, the resistance on the different hot wires changes (some wires become more perpendicular to the freestream, thus cooler; others will align closer to the freestream with less opportunity to cool). By measuring the resistance differences with a bridge, it's possible to derive, angle of attack, sideslip and airspeed. 2. An elliptical body with various pressure ports around the circumference, plus a pitot port. The angle of the flow can be measured by the difference in pressure between the circumference ports (and dividing by the pitot pressure).


Hot wire anemometers are very, very fragile. Installation on aircraft is not practical - a bug strike would render it inoperative.


Talk by the A-12 pilot, Frank Murray. Refers to the SR-71 as the "family model".

https://www.youtube.com/watch?v=MGdxpqqsHl8


YF-12 development film. Check out the avionics test.

https://www.youtube.com/watch?v=Z1FLEbAbl4Q


> From my laymans POV, DNA is just a shit ton of variables in a very complex code that interact with each other. No single point just does a single thing. They all interact with each other. No different than changing a variable in one piece of code and having it create a bug in another that was previously working.

Drew Endy did a lecture this a while ago. It's from one of the chaos computer club seminars.

https://vimeo.com/18201463


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