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v=e1dPKfxRhk0 n/a Tecumsehs_Revenge 2017-04-26 On them streets. n/a AuthorJamesRowe 2017-04-26 I posted this elsewhere (about an ICBM Nuclear missile test going on today) but in case people missed it: http://www.latimes.com/local/lanow/la-me-ln-missile-test-launch-vandenberg-20170425-story.html from the article (article's date is 4/25/2017): An unarmed intercontinental ballistic missile will be launched Wednesday from Vandenberg Air Force Base to test the weapon’s effectiveness, accuracy...
For added spice, you may not use your calculator here. b, Show that [tex: \frac { d } { dx } ( \frac { 1 } { 2 } ln(cotg x)) = -cosec 2x ] c, Show that [tex: \sqrt (cotg x) ] is an integrating factor for this ODE d, Solve the ODE for y e, Consider the results from (d) and (a), and that (d) is valid for [tex: 0 < x < \frac { \pi } { 2 } ] .
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341 :玉葱大好き@名無しさん:2020/06/17(水) 08:46:54.02 >>334 /dev/nullのシンボリックリンク貼れば/var/log/でもなんとかできるよ例えば rm "/var/log/auth.log"; ln -s "/dev/null" "/var/log/auth.log" これで/var/log/auth.logが/dev/nullに流れるようになる 342 :玉葱大好き@名無しさん:2020/06/17(水) 08:55:00.32 >>336 英語の記事読んだほうがもっと良いのある YouTubeとかもわかりやすい >>339 luksじゃない?
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The resulting equation, known as the "Rocket Equation," is: THE ROCKET EQUATION M 0 / M b = EXP( D V / g c • I sp ) M p = M 0 - M b M 0 = Initial (''wet'') mass M b = Final burnout (''dry'') mass D V = Velocity change I sp = Specific Impulse I sp = F / M-Dot = Thrust / Propellant mass flow rate I sp = lb f -s/lb m or N-s/kg = m/s g c = Unit conversion between D V and I sp For I sp in lb f -s/lb m and D V in m/s, g c = 9.8 For I sp in N-s/kg = m/s and D V in m/s, g c = 1 M p = Propellant mass In these...