"In actual rocket nozzles, the exhaust velocity is probably not uniform more than your complete exit cross portion and this sort of velocity profiles are hard to measure precisely. A uniform axial velocity, ve, is assumed for all calculations which use a single-dimensional problem descriptions. This efficient exhaust velocity represents https://edgarfsgte.tokka-blog.com/33268545/how-isp-can-save-you-time-stress-and-money