Adaptation Method for Overall and Local Performances of Gas Turbine Engine Model-Reference-Cited by-同舟云学术

Adaptation Method for Overall and Local Performances of Gas Turbine Engine Model

Published:2018-03 Issue:1 Volume:19 Page:250-261
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:JASS

Author:

Kim Sangjo,Kim Kuisoon,Son Changmin

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/s42405-018-0016-4/fulltext.html

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4. Steinke RJ (1982) STGSTK: a computer code for predicting multistage axial flow compressor performance by a meanline stage stacking method. NASA TP-2020

5. Miller DC, Wasdell DL (1987) Off-design prediction of compressor blade losses. IMechE C279(87):249–260

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