Starting with the integral form of energy conservation [Equations (2.95 and 7.43)], derive an expression for energy
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Starting with the integral form of energy conservation [Equations (2.95 and 7.43)], derive an expression for energy conservation in a steady, inviscid, nonchemically reacting flow without body forces along a streamline that passes through a compressor or turbine. Use \(W_{\text {shaft }}\) to represent the work done on the system by the compressor or turbine per unit mass of flow in \(J / \mathrm{kg}\). Your result should be analogous to Equation (7.53) or (7.54) except that the total enthalpy will not be constant.
2.95:
7.43:
7.53:
7.54:
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Related Book For
Fundamentals Of Aerodynamics ISE
ISBN: 9781266076442
7th Edition
Authors: John D. Anderson, Jr, Christopher P Cadou
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