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Gene Messercola, Pete Costigan, Intesar Hoque Jet Engines achieve propulsion from thrust created by hot gas exiting the Brayton Cycle.

Published byLoreen Briggs Modified over 9 years ago

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Presentation on theme: "Gene Messercola, Pete Costigan, Intesar Hoque Jet Engines achieve propulsion from thrust created by hot gas exiting the Brayton Cycle."— Presentation transcript:

1 Gene Messercola, Pete Costigan, Intesar Hoque Jet Engines achieve propulsion from thrust created by hot gas exiting the Brayton Cycle.

2 1→2: Isentropic Compression 2→3: Reversible Constant Pressure Heat Addition 3→4: Isentropic Expansion 4→1: Reversible Constant Pressure Heat Rejection (Exhaust and Intake in the open cycle) Air is compressed, mixed with fuel, burned, and expelled through a turbine to perform work. Lab analysis includes the calculation of work and efficiency of the turbine and compressor as well as Carnot efficiency.

3  Thrust to lift a human /Thrust of the jet turbine  Analyze heat transfer of the turbine  Determine if a scaled model is viable heat wise  What sort of material would be needed to insulate from the body  Is this feasible for personal flight? Our Experiment

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