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Unformatted text preview: efficiency, overall efficiency, and TSFC. Know the Brequet range equation and be able to use it to determine the effect of engine performance on range. 4. Be able to analyze the performance of the following components, given efficiencies and adequate boundary conditions: a. Inlets; subsonic and supersonic and all combinations b. Compressors and fans c. Combustors or burners d. Turbines e. Nozzles 5. Be able to sketch the T-s diagrams representing the performance of each component and identify real and ideal states. 6. Be able to sketch the T-s diagrams for each type of airbreathing engine we discussed. 7. Be able to determine the principal performance parameters (T/m a , TSFC, p , th , and o for each of the engines we discussed....
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- Fall '08