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Recent CFD applications in small gas turbine combustion systems developmentA typical small gas turbine combustor is modelled using CFD, and the numerical results are compared with laser doppler velocimetry (LDV) measured data. The predicted flow characteristics are in excellent agreement with the measurements. Some aspects of CFD application in combustor design are discussed. CFD can be used in the following ways: as a tool in studying the flowfield development; in the optimization of location, size, and quantity of flow devices; in monitoring flow performance; and in correlating important design parameters. Use of CFD can significantly reduce the lapse time and the development cost of gas turbine combustors.

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Document ID
19940024754
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
External Source(s)
https://www.sto.nato.int/document/fuels-and-combustion-technology-for-advanced-aircraft-engines/
Authors
T. C. J. Hu (Pratt & Whitney)
L. A. Prociw (Pratt & Whitney)
Date Acquired
August 16, 2013
Publication Date
September 1, 1993
Publication Information
Publication: AGARD, Fuels and Combustion Technology for Advanced Aircraft Engines
Publisher: North Atlantic Treaty Organization
ISBN: 92-835-0719-3
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AGARD-CP-536
AD-A275679
Meeting Information
Meeting: The Propulsion and Energetics Panel 81st Symposium
Location: Fiuggi
Country: IT
Start Date: May 10, 1993
End Date: May 14, 1993
Sponsors: North Atlantic Treaty Organization
Accession Number
94N29257
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Controlled, Proprietary or Sensitive Information:
  • Limited Distribution
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IDRelationTitle19940024743Collected WorksFuels and Combustion Technology for Advanced Aircraft Engines [Les Propergols et les Systèmes de Combustion pour les Moteurs d'Aéronefs]
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