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Autor:
Kirk Gallier, Arman Mirhashemi, Greg Sluyter, Joshua Szczudlak, Sara Rostami, Gregory M. Laskowski, Scott C. Morris, Jon Slepski
Publikováno v:
Volume 2B: Turbomachinery.
Flow exiting the combustor is highly turbulent and contains significant spatial gradients of pressure and temperature. The high pressure turbine nozzle vanes operating in this environment redistribute these spatial gradients and impact the inflow cha
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::348c3d10d4688a0adb5393e5e2af0c2c
https://doi.org/10.1115/gt2018-77281
https://doi.org/10.1115/gt2018-77281
