Aerodynamic Performance of Multi-stage Axial Compressor Considering Cold-to-Hot Deformation Effect-Reference-Cited by-同舟云学术

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Aerodynamic Performance of Multi-stage Axial Compressor Considering Cold-to-Hot Deformation Effect

Published:2018-07-04 Issue:3 Volume:19 Page:651-660
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Kim Sangjo,Kim Kuisoon,Son Changmin

Funder

Human Resources Development program

Korea Institute of Energy Technology Evaluation and Planning (KETEP) and the Ministry of Trade, Industry & Energy (MOTIE) of the Republic of Korea

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

http://link.springer.com/article/10.1007/s42405-018-0051-1/fulltext.html

Reference27 articles.

1. UNFCCC (2015) Adoption of the Paris agreement (1/CP.21). United Nations Framework Convention on Climate Change, Bonn

2. Pan X, den Elzen M, Höhne N, Teng F, Wang L (2017) Exploring fair and ambitious mitigation contributions under the Paris agreement goals. Environ Sci Policy 74:49–56

3. Graham WR, Hall CA, Morales MV (2014) The potential of future aircraft technology for noise and pollutant emissions reduction. Transp Policy 34:36–51

4. Gallar L, Arias M, Pachidis V, Singh R (2011) Stochastic axial compressor variable geometry schedule optimization. Aerosp Sci Technol 15(5):366–374

5. Kim S, Kim D, Son C, Kim K, Kim M, Min S (2015) A full engine cycle analysis of a turbofan engine for optimum scheduling of variable guide vanes. Aerosp Sci Technol 47:21–30

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2. Equivalent model for an axial compressor used for aero engines based on 1D and 3D analytical models and performance data;Aerospace Science and Technology;2022-02

3. A new performance adaptation method for aero gas turbine engines based on large amounts of measured data;Energy;2021-04

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