Aerothermodynamics optimal design of a multistage axial compressor in a gas turbine using directly manipulated free-form deformation-Reference-Cited by-同舟云学术

Aerothermodynamics optimal design of a multistage axial compressor in a gas turbine using directly manipulated free-form deformation

Published:2021-08 Issue: Volume:26 Page:101142
ISSN:2214-157X
Container-title:Case Studies in Thermal Engineering
language:en
Short-container-title:Case Studies in Thermal Engineering

Author:

Xiang Hang,Chen Jiang

Funder

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Engineering (miscellaneous)

Reference25 articles.

1. Prediction of off Design Performance of Multistage Compressors, NASA SP-36. Charpter X;Robbins,1965

2. Overall and stage characteristics of axial-flow compressors;Howell,1950

3. Flow field and performance map computations for axial-flow compressors and turbines;Novak;AGARD (Advis. Group Aerosp. Res. Dev.) Lect. Ser.,1976

4. Compressor and turbine performance prediction system development-lessons from thirty years of history;Serovy;AGARD (Advis. Group Aerosp. Res. Dev.) Lect. Ser.,1976

5. Axial flow compressor performance prediction;Wall;AGARD (Advis. Group Aerosp. Res. Dev.) Lect. Ser.,1976

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