Bridging the gap between structural and thermal analysis in aircraft engine design-Reference-Cited by-同舟云学术

Bridging the gap between structural and thermal analysis in aircraft engine design

Published:2000-09-06 Issue: Volume: Page:
ISSN:
Container-title:8th Symposium on Multidisciplinary Analysis and Optimization
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Author:

Ebert E.,Reile E.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4782

Reference4 articles.

1. Dixon J. A. "Gas Turbine Critical Component Temperature Predictions for Fatigue Life and Integrity Considerations". Technical Report ISABE-99-7117, ISABE 14th International Symposium on Air Breathing Engines, Florence, Italy, September 1999.

2. Monico R. D. and Chew J. W. "Thermal Behavior ofTurbomachinery Discs and Casings". Technical Report AGARD-CP-527, AGARD Heat Transfer and Cooling in Gas Turbines, Antalya, Turkey, February 1993.

3. Reile E. "MSC/PATRAN-Integriertes Thermal - Analyse - System bei der MTU". Technicalreport,MSC-User Conference, Bad Neuenahr, Germany, June 1997.

4. Hennecke D. K. and Trappmann K. "Turbine Tip-Clearancein Gas Turbine Engines". Technical Report AGARD CP-324, AGARD 60th Symposium on 'Engine Handling', Marathon, Greece, October 1982.

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