Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference7 articles.
1. Steady-State Modeling of Gas Turbine Engines Using the Numerical Propulsion System Simulation Code
2. 3Paxson,D.E."ASimplifiedModelforDetonationBasedPressure-GainCombustors,"AIAA2010-6717,July2010.
3. 4Paxson, D. E., and Kaemming, T. A. "Foundational Performance Analyses of Pressure Gain Combustion Thermodynamic Benefits for GasTurbines,"AIAA2012-0770,January2012.
4. 5Nickol,C.L."HybridWingBodyConfigurationScalingStudy,"AIAA2012-0337,January2012
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