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NASA Thrust Equation gets destroyed.
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In accordance with industry accepted best practices we ask that users limit their copy / paste of copyrighted material to the relevant portions of the article you wish to discuss and no more than 50% of the source material, provide a link back to the original article and provide your original comments / criticism in your post with the article.
[quote:Anonymous Coward 73811843:MV8zOTg5OTIyXzcyMjIyNDc4X0Q2RDY0QzRC] [quote:Anonymous Coward 76708078:MV8zOTg5OTIyX0ZCRDQ1NzdE] [youtube]https://www.youtube.com/watch?v=zOm04TkpViQ&feature=youtu.be[/youtube] [/quote] He says the combined and reduced formula no longer needed exit velocity for the equation, but velocity is contained in flow rate. Distance/time is contained in the first equation listed in the fluid dynamics group of three. I assume constant velocity, because a venturi was never mentioned. Therefore flow rate is exit velocity in different units times pipe area. Plus let go of a fire hose to see mass of fluid times velocity does equal force. [/quote]
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