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Thank You! Yes I saw the reference to Eqn 7.11, but tried using 7.11a as 1/[pi*Po1*ao1^3] where ao1 = sqrt(gamma*R*To1). I appreciate your help! Thanks again. David "Pete K." <[EMAIL PROTECTED]> wrote in message news:<[EMAIL PROTECTED]>... > Did you miss the reference to Eqn 7.11? The LHS of the eqn is > mdot*Omega^2/[pi*k*gamma*Po1*sqrt(gamma*R*To1)]. If you take out > mdot*omega^2/k, what's left, > 1/[pi*gamma*Po1*sqrt(gamma*R*To1)], is equal to 0.6598e-8. Did you actually > try to plug in numbers? > > Pete K. > > "David Walden" <[EMAIL PROTECTED]> wrote in message > news:[EMAIL PROTECTED] > > A solution to problem 7.4 in SL Dixon's Fluid Mechanics and > > Thermodynamics of Turbomachinery 4th Ed. has me stumped and I would > > appreciate any help understanding the steps that were left out. > > > > "The compressible flow relation between mass flow rate, speed of > > rotation and the flow parameters at the eye tip is given by eqn. > > (7.11), > > > > 0.6598 x 10^-8 x (mdot x rads ^2)/k = ..." > > > > I've not figured out yet how we're to get 0.6598 x 10^-8 > > > > Thanks for your time, > > > > David
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