Dynamic Modeling, Simulation, and Controls of a SOFC Combustor Hybrid Cycle for Commercial Electric Aviation
Author:
Affiliation:
1. Tennessee Tech University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1461
Reference24 articles.
1. Transient Analysis of an Innovative Cycle Integrating a SOFC and a Turbogenerator for Electric Propulsion
2. Surge Margin Optimization of Centrifugal Compressors Using a New Objective Function Based on Local Flow Parameters
3. Reid, L. & Moore, R. D. (1978). Performance of Single-Stage Axial-Flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and With Design Pressure Ratio of 1.82. https://ntrs.nasa.gov/api/citations/19790001889/downloads/19790001889.pdf
4. Modeling and analysis of autothermal reforming of methane to hydrogen in a fixed bed reformer
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