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:

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7.43:

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7.53:

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7.54:

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Fundamentals Of Aerodynamics ISE

ISBN: 9781266076442

7th Edition

Authors: John D. Anderson, Jr, Christopher P Cadou

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