Prediction of gas turbine combustor flow by a finite element code-Reference-Cited by-同舟云学术

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Prediction of gas turbine combustor flow by a finite element code

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

LENTINI D.¹,FELIZIANI C.¹,IONTA P.¹,RISPOLI F.¹

Affiliation:

1. Roma I, Universita,Rome, Italy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3469

Reference39 articles.

1. Sturgess G.J., Sloan D.G., Roquemore W.M., Reddy V.K., Shouse D., Leamerises A.L., Ballal D.R., Heneghan S.P., VangsnessM.D. and Hedman P.O. Tlame Stability and LeanBlowout A Research Program ProQess in Proc. 1Oth ISABE,Nottingham, England, 1991,pp.372-384.

2. Impact of Nurnerical Methods on Gas Turbine Combustor Design and Development

3. Computation of Flow in a Gas Turbine Combustor

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