• Engineering
  • Published 2007

Novel turbomachinery concepts for highly integrated airframe/propulsion systems

@inproceedings{Shah2007NovelTC,
  title={Novel turbomachinery concepts for highly integrated airframe/propulsion systems},
  author={Parthiv N. Shah},
  year={2007}
}
Two novel turbomachinery concepts are presented as enablers to advanced flight missions requiring integrated airframe/propulsion systems. The first concept is motivated by thermal management challenges in low-to-high Mach number (4+) aircraft. The idea of compressor cooling combines the compressor and heat exchanger function to stretch turbopropulsion system operational limits. Axial compressor performance with blade passage heat extraction is assessed with computational experiments and… CONTINUE READING

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