Performance Cycle Analysis of Turbofan Engine with Interstage Turbine Burner
Author:
Affiliation:
1. Michigan Technological University, Houghton, Michigan 49931-1295
2. Mattingly Consulting, Bothell, Washington 98011
3. NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.13394
Reference11 articles.
1. 1Zucrow, M. J., Aircraft and Missile Propulsion: VolumeII, Wiley, New York, 1964, pp.52, 53.
2. Parametric Cycle Analysis of a Turbofan Engine with an Interstage Turbine Burner
3. Turbojet and Turbofan Engine Performance Increases Through Turbine Burners
4. Performance Increases for Gas-Turbine Engines Through Combustion Inside the Turbine
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