Automated thermal and stress preliminary analyses applied to a turbine rotor-Reference-Cited by-同舟云学术

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Automated thermal and stress preliminary analyses applied to a turbine rotor

Published:2017-04 Issue: Volume:63 Page:123-131
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Moret Maxime,Delecourt Alexandre,Moustapha Hany,Abenhaim Acher-Igal,Garnier Francois

Funder

Pratt and Whitney Canada

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. Chapter 3: Air Vehicles;NATO Science and Technology Organization,2006

2. Preliminary multi-disciplinary optimization in turbomachinery design;Panchenko,2002

3. Multidisciplinary design optimization: a survey of architectures;Martins;AIAA J.,2013

4. Multidisciplinary Optimization Methods for Preliminary Design;Korte,1998

5. High-pressure-turbine clearance control systems: current practices and future directions;Lattime;J. Propuls. Power,2004

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1. A new method to identify non-steady thermal load based on element differential method;International Journal of Heat and Mass Transfer;2023-10

2. Dual-convolutional neural network based aerodynamic prediction and multi-objective optimization of a compact turbine rotor;Aerospace Science and Technology;2021-09

3. Identification of the transient temperature and stress distribution in an atmospheric reentry capsule assuming temperature-dependent material properties;Aerospace Science and Technology;2017-08

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