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Consider a laminar boundary layer developing over an isothermal flat plate. The flow is incompressible, and viscous dissipation is negligible.
(a) Substitute Equations 6.31 and 6.33 into Equation 6.39 to determine the thermal boundary conditions in dimensional form associated with flow over a flat plate of length L and temperature Ts.
(b) Substitute Equations 6.31, 6.32, and 6.33, as well as the definitions of ReL and Pr, into Equation 6.36, and compare the resulting dimensional expression with Equation 6.29.
develop equations which may be solved to give the final temperature of the gas remaining in a tank after the tank has
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An amount P must be invested now to allow withdrawals of $1,000 per year for the next 15 years and to permit $300 to be withdrawn starting at the end of year 6 and continuing over the remainder of the 15-year period as the $300 increases by 6% per ye..
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