Gas Turbine Combustor Modeling with and without Nozzle Guide Vanes attached.

From National Research Council Canada

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Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
  2. Mecachrome Technologies Inc.
FormatText, Article
ConferenceASME Turbo Expo 2009 June 8-12, 2009. From June 8 to June 12, 2009, Orlanda, Fl, USA
Subjectmicro gas turbine engine; combustor modeling; combustor and turbine coupling
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberGTL-2008-0040
NPARC number8930061
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Record identifierb6351f1e-71db-4d91-86ff-0f1e7c73c5bc
Record created2009-04-23
Record modified2020-04-16
Date modified: