Exploring the Effects of Removing Process-Intrinsic Constraints on Gas Turbine Design

Author:

Bell Theo A.1,Jarrett Jerome P.1,Clarkson P. John1

Affiliation:

1. University of Cambridge, Cambridge, England CB2 1PZ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference43 articles.

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A Medial-Object-based Design-in-Context Approach for the Structural Design of Engine Subsystems;AIAA Propulsion and Energy 2019 Forum;2019-08-16

2. Evaluation of Gas Turbine Outboard Bleed Air on Overall Engine Efficiency and CO2e Emission in Natural Gas Compressor Stations;Journal of Engineering for Gas Turbines and Power;2013-08-30

3. An Approach to Multi-fidelity Optimization of Aeroengine Compression Systems;12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2012-09-11

4. Robust Design Optimization of Gas Turbine Compression Systems;Journal of Propulsion and Power;2011-03

5. An Integrated System for the Aerodynamic Design of Compression Systems—Part II: Application;Journal of Turbomachinery;2010-09-21

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